3 values: ["DEFAULT", "CW0", "CW90", "CW180", "CW270", "CW0FLIP", "CW90FLIP", "CW180FLIP", "CW270FLIP"]
5 values: ["NONE", "AUTO", "MPU6000", "MPU6500", "MPU9250", "BMI160", "ICM20689", "BMI088", "ICM42605", "BMI270","LSM6DXX", "FAKE"]
6 enum: accelerationSensor_e
7 - name: rangefinder_hardware
8 values: ["NONE", "SRF10", "VL53L0X", "MSP", "BENEWAKE", "VL53L1X", "US42", "TOF10120_I2C", "FAKE", "TERARANGER_EVO", "USD1_V0", "NRA"]
9 enum: rangefinderType_e
11 values: ["NONE", "AUTO", "HMC5883", "AK8975", "MAG3110", "AK8963", "IST8310", "QMC5883", "MPU9250", "IST8308", "LIS3MDL", "MSP", "RM3100", "VCM5883", "MLX90393", "FAKE"]
13 - name: opflow_hardware
14 values: ["NONE", "CXOF", "MSP", "FAKE"]
15 enum: opticalFlowSensor_e
17 values: ["NONE", "AUTO", "BMP085", "MS5611", "BMP280", "MS5607", "LPS25H", "SPL06", "BMP388", "DPS310", "B2SMPB", "MSP", "FAKE"]
19 - name: pitot_hardware
20 values: ["NONE", "AUTO", "MS4525", "ADC", "VIRTUAL", "FAKE", "MSP", "DLVR-L10D"]
23 values: ["NONE", "SERIAL", "MSP", "SIM (SITL)"]
24 enum: rxReceiverType_e
26 values: ["SPEK1024", "SPEK2048", "SBUS", "SUMD", "IBUS", "JETIEXBUS", "CRSF", "FPORT", "SBUS_FAST", "FPORT2", "SRXL2", "GHST", "MAVLINK", "FBUS", "SBUS2"]
27 - name: blackbox_device
28 values: ["SERIAL", "SPIFLASH", "SDCARD", "FILE"]
29 - name: motor_pwm_protocol
30 values: ["STANDARD", "ONESHOT125", "MULTISHOT", "BRUSHED", "DSHOT150", "DSHOT300", "DSHOT600"]
31 - name: servo_protocol
32 values: ["PWM", "SBUS", "SBUS_PWM"]
33 - name: failsafe_procedure
34 values: ["LAND", "DROP", "RTH", "NONE"]
35 - name: current_sensor
36 values: ["NONE", "ADC", "VIRTUAL", "FAKE", "ESC"]
38 - name: voltage_sensor
39 values: ["NONE", "ADC", "ESC", "FAKE"]
41 - name: imu_inertia_comp_method
42 values: ["VELNED", "TURNRATE","ADAPTIVE"]
43 enum: imu_inertia_comp_method_e
45 values: ["UBLOX", "MSP", "FAKE"]
48 values: ["AUTO", "EGNOS", "WAAS", "MSAS", "GAGAN", "SPAN", "NONE"]
51 values: ["PEDESTRIAN","AUTOMOTIVE", "AIR_1G", "AIR_2G", "AIR_4G", "SEA", "MOWER"]
54 values: ["NEVER", "FIRST_ARM", "EACH_ARM"]
56 values: ["RIGHT", "LEFT", "YAW"]
57 - name: nav_user_control_mode
58 values: ["ATTI", "CRUISE"]
59 - name: nav_rth_alt_mode
60 values: ["CURRENT", "EXTRA", "FIXED", "MAX", "AT_LEAST"]
61 - name: nav_rth_climb_first_stage_modes
62 values: ["AT_LEAST", "EXTRA"]
64 values: ["IMPERIAL", "METRIC", "METRIC_MPH", "UK", "GA"]
66 - name: osd_stats_energy_unit
68 enum: osd_stats_energy_unit_e
69 - name: osd_video_system
70 values: ["AUTO", "PAL", "NTSC", "HDZERO", "DJIWTF", "AVATAR", "BF43COMPAT", "BFHDCOMPAT"]
73 values: ["OFF", "ON","TEST"]
76 values: ["LEFT", "RIGHT"]
79 values: ["NORMAL", "MEDIUM", "SLOW"]
81 values: ["400KHZ", "800KHZ", "100KHZ", "200KHZ"]
83 values: ["NONE", "AGL", "FLOW_RAW", "FLOW", "ALWAYS", "SAG_COMP_VOLTAGE",
84 "VIBE", "CRUISE", "REM_FLIGHT_TIME", "SMARTAUDIO", "ACC",
85 "NAV_YAW", "PCF8574", "DYN_GYRO_LPF", "AUTOLEVEL", "ALTITUDE",
86 "AUTOTRIM", "AUTOTUNE", "RATE_DYNAMICS", "LANDING", "POS_EST",
87 "ADAPTIVE_FILTER", "HEADTRACKER", "GPS", "LULU", "SBUS2"]
90 enum: modeActivationOperator_e
91 - name: osd_crosshairs_style
92 values: ["DEFAULT", "AIRCRAFT", "TYPE3", "TYPE4", "TYPE5", "TYPE6", "TYPE7", "TYPE8"]
93 enum: osd_crosshairs_style_e
94 - name: osd_sidebar_scroll
95 values: ["NONE", "ALTITUDE", "SPEED", "HOME_DISTANCE"]
96 enum: osd_sidebar_scroll_e
97 - name: nav_rth_allow_landing
98 values: ["NEVER", "ALWAYS", "FS_ONLY"]
99 enum: navRTHAllowLanding_e
100 - name: bat_capacity_unit
101 values: ["MAH", "MWH"]
102 enum: batCapacityUnit_e
103 - name: bat_voltage_source
104 values: ["RAW", "SAG_COMP"]
105 enum: batVoltageSource_e
106 - name: smartport_fuel_unit
107 values: ["PERCENT", "MAH", "MWH"]
108 enum: smartportFuelUnit_e
109 - name: platform_type
110 values: ["MULTIROTOR", "AIRPLANE", "HELICOPTER", "TRICOPTER", "ROVER", "BOAT"]
111 - name: tz_automatic_dst
112 values: ["OFF", "EU", "USA"]
113 enum: tz_automatic_dst_e
114 - name: vtx_low_power_disarm
115 values: ["OFF", "ON", "UNTIL_FIRST_ARM"]
116 enum: vtxLowerPowerDisarm_e
117 - name: vtx_frequency_groups
118 values: ["FREQUENCYGROUP_5G8", "FREQUENCYGROUP_2G4", "FREQUENCYGROUP_1G3"]
119 enum: vtxFrequencyGroups_e
121 values: ["PT1", "BIQUAD"]
122 - name: filter_type_full
123 values: ["PT1", "BIQUAD", "PT2", "PT3", "LULU"]
125 values: ["ERROR", "WARNING", "INFO", "VERBOSE", "DEBUG"]
127 values: ["OFF", "RP", "RPY"]
129 - name: airmodeHandlingType
130 values: ["STICK_CENTER", "THROTTLE_THRESHOLD", "STICK_CENTER_ONCE"]
131 - name: nav_extra_arming_safety
132 values: ["ON", "ALLOW_BYPASS"]
133 enum: navExtraArmingSafety_e
135 values: ["NONE", "AUTO", "ADC", "CHANNEL", "PROTOCOL", "MSP"]
138 values: ["NONE", "PID", "PIFF", "AUTO"]
140 - name: osd_ahi_style
141 values: ["DEFAULT", "LINE"]
142 enum: osd_ahi_style_e
145 values: ["AUTO", "ON", "OFF"]
146 - name: osd_crsf_lq_format
147 enum: osd_crsf_lq_format_e
148 values: ["TYPE1", "TYPE2", "TYPE3"]
150 values: ["OFF", "ON"]
151 - name: djiOsdTempSource
152 values: ["ESC", "IMU", "BARO"]
153 enum: djiOsdTempSource_e
154 - name: osdSpeedSource
155 values: ["GROUND", "3D", "AIR"]
156 enum: osdSpeedSource_e
157 - name: nav_overrides_motor_stop
158 enum: navOverridesMotorStop_e
159 values: ["OFF_ALWAYS", "OFF", "AUTO_ONLY", "ALL_NAV"]
160 - name: osd_plus_code_short
161 values: ["0", "2", "4", "6"]
162 - name: autotune_rate_adjustment
163 enum: autotune_rate_adjustment_e
164 values: ["FIXED", "LIMIT", "AUTO"]
165 - name: safehome_usage_mode
166 values: ["OFF", "RTH", "RTH_FS"]
167 enum: safehomeUsageMode_e
168 - name: nav_rth_climb_first
169 enum: navRTHClimbFirst_e
170 values: ["OFF", "ON", "ON_FW_SPIRAL"]
171 - name: nav_wp_mission_restart
172 enum: navMissionRestart_e
173 values: ["START", "RESUME", "SWITCH"]
174 - name: djiRssiSource
175 values: ["RSSI", "CRSF_LQ"]
176 enum: djiRssiSource_e
177 - name: rth_trackback_mode
178 values: ["OFF", "ON", "FS"]
179 enum: rthTrackbackMode_e
180 - name: dynamic_gyro_notch_mode
182 enum: dynamicGyroNotchMode_e
183 - name: nav_fw_wp_turn_smoothing
184 values: ["OFF", "ON", "ON-CUT"]
185 enum: wpFwTurnSmoothing_e
186 - name: gps_auto_baud_max
187 values: [ '115200', '57600', '38400', '19200', '9600', '230400', '460800', '921600']
189 - name: nav_mc_althold_throttle
190 values: ["STICK", "MID_STICK", "HOVER"]
191 enum: navMcAltHoldThrottle_e
192 - name: led_pin_pwm_mode
193 values: ["SHARED_LOW", "SHARED_HIGH", "LOW", "HIGH"]
194 enum: led_pin_pwm_mode_e
195 - name: gyro_filter_mode
196 values: ["OFF", "STATIC", "DYNAMIC", "ADAPTIVE"]
197 enum: gyroFilterType_e
198 - name: headtracker_dev_type
199 values: ["NONE", "SERIAL", "MSP"]
200 enum: headTrackerDevType_e
201 - name: mavlink_radio_type
202 values: ["GENERIC", "ELRS", "SIK"]
204 - name: default_altitude_source
205 values: ["GPS", "BARO", "GPS_ONLY", "BARO_ONLY"]
206 enum: navDefaultAltitudeSensor_e
215 ROLL_PITCH_RATE_MIN: 4
216 ROLL_PITCH_RATE_MAX: 180
218 MAX_CONTROL_RATE_PROFILE_COUNT: 3
219 MAX_BATTERY_PROFILE_COUNT: 3
223 - name: PG_GYRO_CONFIG
225 headers: ["sensors/gyro.h"]
228 description: "This is the main loop time (in us). Changing this affects PID effect with some PID controllers (see PID section for details). A very conservative value of 3500us/285Hz should work for everyone. Setting it to zero does not limit loop time, so it will go as fast as possible."
231 - name: gyro_anti_aliasing_lpf_hz
232 description: "Gyro processing anti-aliasing filter cutoff frequency. In normal operation this filter setting should never be changed. In Hz"
234 field: gyro_anti_aliasing_lpf_hz
236 - name: gyro_lulu_enabled
237 description: "Enable/disable gyro LULU filter"
239 field: gyroLuluEnabled
241 - name: gyro_lulu_sample_count
242 description: "Gyro lulu sample count, in number of samples."
244 field: gyroLuluSampleCount
247 - name: gyro_main_lpf_hz
248 description: "Software based gyro main lowpass filter. Value is cutoff frequency (Hz)"
250 field: gyro_main_lpf_hz
253 - name: gyro_filter_mode
254 description: "Specifies the type of the software LPF of the gyro signals."
255 default_value: "STATIC"
256 field: gyroFilterMode
257 table: gyro_filter_mode
258 - name: gyro_dyn_lpf_min_hz
259 description: "Minimum frequency of the gyro Dynamic LPF"
261 field: gyroDynamicLpfMinHz
264 - name: gyro_dyn_lpf_max_hz
265 description: "Maximum frequency of the gyro Dynamic LPF"
267 field: gyroDynamicLpfMaxHz
270 - name: gyro_dyn_lpf_curve_expo
271 description: "Expo value for the throttle-to-frequency mapping for Dynamic LPF"
273 field: gyroDynamicLpfCurveExpo
276 - name: dynamic_gyro_notch_enabled
277 description: "Enable/disable dynamic gyro notch also known as Matrix Filter"
279 field: dynamicGyroNotchEnabled
280 condition: USE_DYNAMIC_FILTERS
282 - name: dynamic_gyro_notch_q
283 description: "Q factor for dynamic notches"
285 field: dynamicGyroNotchQ
286 condition: USE_DYNAMIC_FILTERS
289 - name: dynamic_gyro_notch_min_hz
290 description: "Minimum frequency for dynamic notches. Default value of `150` works best with 5\" multirotors. Should be lowered with increased size of propellers. Values around `100` work fine on 7\" drones. 10\" can go down to `60` - `70`"
292 field: dynamicGyroNotchMinHz
293 condition: USE_DYNAMIC_FILTERS
296 - name: dynamic_gyro_notch_mode
297 description: "Gyro dynamic notch type"
299 table: dynamic_gyro_notch_mode
300 field: dynamicGyroNotchMode
301 condition: USE_DYNAMIC_FILTERS
302 - name: dynamic_gyro_notch_3d_q
303 description: "Q factor for 3D dynamic notches"
305 field: dynamicGyroNotch3dQ
306 condition: USE_DYNAMIC_FILTERS
310 description: "On multi-gyro targets, allows to choose which gyro to use. 0 = first gyro, 1 = second gyro"
311 condition: USE_DUAL_GYRO
315 - name: setpoint_kalman_enabled
316 description: "Enable Kalman filter on the gyro data"
318 condition: USE_GYRO_KALMAN
321 - name: setpoint_kalman_q
322 description: "Quality factor of the setpoint Kalman filter. Higher values means less filtering and lower phase delay. On 3-7 inch multirotors can be usually increased to 200-300 or even higher of clean builds"
325 condition: USE_GYRO_KALMAN
328 - name: init_gyro_cal
329 description: "If defined to 'OFF', it will ignore the gyroscope calibration done at each startup. Instead, the gyroscope last calibration from when you calibrated will be used. It also means you don't have to keep the UAV stationary during a startup."
331 field: init_gyro_cal_enabled
334 description: "Calculated gyro zero calibration of axis X"
336 field: gyro_zero_cal[X]
340 description: "Calculated gyro zero calibration of axis Y"
342 field: gyro_zero_cal[Y]
346 description: "Calculated gyro zero calibration of axis Z"
348 field: gyro_zero_cal[Z]
351 - name: ins_gravity_cmss
352 description: "Calculated 1G of Acc axis Z to use in INS"
354 field: gravity_cmss_cal
357 - name: gyro_adaptive_filter_target
358 description: "Target value for adaptive filter"
360 field: adaptiveFilterTarget
363 condition: USE_ADAPTIVE_FILTER
364 - name: gyro_adaptive_filter_min_hz
365 description: "Minimum frequency for adaptive filter"
367 field: adaptiveFilterMinHz
370 condition: USE_ADAPTIVE_FILTER
371 - name: gyro_adaptive_filter_max_hz
372 description: "Maximum frequency for adaptive filter"
374 field: adaptiveFilterMaxHz
377 condition: USE_ADAPTIVE_FILTER
378 - name: gyro_adaptive_filter_std_lpf_hz
379 description: "Standard deviation low pass filter cutoff frequency"
381 field: adaptiveFilterStdLpfHz
384 condition: USE_ADAPTIVE_FILTER
385 - name: gyro_adaptive_filter_hpf_hz
386 description: "High pass filter cutoff frequency"
388 field: adaptiveFilterHpfHz
391 condition: USE_ADAPTIVE_FILTER
392 - name: gyro_adaptive_filter_integrator_threshold_high
393 description: "High threshold for adaptive filter integrator"
395 field: adaptiveFilterIntegratorThresholdHigh
398 condition: USE_ADAPTIVE_FILTER
399 - name: gyro_adaptive_filter_integrator_threshold_low
400 description: "Low threshold for adaptive filter integrator"
402 field: adaptiveFilterIntegratorThresholdLow
405 condition: USE_ADAPTIVE_FILTER
407 - name: PG_ADC_CHANNEL_CONFIG
408 type: adcChannelConfig_t
409 headers: ["fc/config.h"]
412 - name: vbat_adc_channel
413 description: "ADC channel to use for battery voltage sensor. Defaults to board VBAT input (if available). 0 = disabled"
414 default_value: :target
415 field: adcFunctionChannel[ADC_BATTERY]
418 - name: rssi_adc_channel
419 description: "ADC channel to use for analog RSSI input. Defaults to board RSSI input (if available). 0 = disabled"
420 default_value: :target
421 field: adcFunctionChannel[ADC_RSSI]
424 - name: current_adc_channel
425 description: "ADC channel to use for analog current sensor input. Defaults to board CURRENT sensor input (if available). 0 = disabled"
426 default_value: :target
427 field: adcFunctionChannel[ADC_CURRENT]
430 - name: airspeed_adc_channel
431 description: "ADC channel to use for analog pitot tube (airspeed) sensor. If board doesn't have a dedicated connector for analog airspeed sensor will default to 0"
432 default_value: :target
433 field: adcFunctionChannel[ADC_AIRSPEED]
437 - name: PG_ACCELEROMETER_CONFIG
438 type: accelerometerConfig_t
439 headers: ["sensors/acceleration.h"]
442 description: "Frequency of the software notch filter to remove mechanical vibrations from the accelerometer measurements. Value is center frequency (Hz)"
446 - name: acc_notch_cutoff
447 description: "Frequency of the software notch filter to remove mechanical vibrations from the accelerometer measurements. Value is cutoff frequency (Hz)"
452 description: "Selection of acc hardware. See Wiki Sensor auto detect and hardware failure detection for more info"
453 default_value: "AUTO"
456 description: "Software-based filter to remove mechanical vibrations from the accelerometer measurements. Value is cutoff frequency (Hz). For larger frames with bigger props set to lower value."
461 description: "Specifies the type of the software LPF of the acc signals. BIQUAD gives better filtering and more delay, PT1 less filtering and less delay, so use only on clean builds."
462 default_value: "BIQUAD"
463 field: acc_soft_lpf_type
466 description: "Calculated value after '6 position avanced calibration'. See Wiki page."
468 field: accZero.raw[X]
472 description: "Calculated value after '6 position avanced calibration'. See Wiki page."
474 field: accZero.raw[Y]
478 description: "Calculated value after '6 position avanced calibration'. See Wiki page."
480 field: accZero.raw[Z]
484 description: "Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page."
486 field: accGain.raw[X]
490 description: "Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page."
492 field: accGain.raw[Y]
496 description: "Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page."
498 field: accGain.raw[Z]
502 - name: PG_RANGEFINDER_CONFIG
503 type: rangefinderConfig_t
504 headers: ["sensors/rangefinder.h"]
505 condition: USE_RANGEFINDER
507 - name: rangefinder_hardware
508 table: rangefinder_hardware
509 description: "Selection of rangefinder hardware."
510 default_value: "NONE"
511 - name: rangefinder_median_filter
512 description: "3-point median filtering for rangefinder readouts"
514 field: use_median_filtering
517 - name: PG_OPFLOW_CONFIG
518 type: opticalFlowConfig_t
519 headers: ["sensors/opflow.h"]
520 condition: USE_OPFLOW
522 - name: opflow_hardware
523 description: "Selection of OPFLOW hardware."
525 table: opflow_hardware
527 description: "Optical flow module scale factor"
532 description: "Optical flow module alignment (default CW0_DEG_FLIP)"
533 default_value: CW0FLIP
538 - name: PG_COMPASS_CONFIG
539 type: compassConfig_t
540 headers: ["sensors/compass.h"]
544 description: "When running on non-default hardware or adding support for new sensors/sensor boards, these values are used for sensor orientation. When carefully understood, these values can also be used to rotate (in 90deg steps) or flip the board. Possible values are: DEFAULT, CW0_DEG, CW90_DEG, CW180_DEG, CW270_DEG, CW0_DEG_FLIP, CW90_DEG_FLIP, CW180_DEG_FLIP, CW270_DEG_FLIP."
545 default_value: "DEFAULT"
550 description: "Selection of mag hardware. See Wiki Sensor auto detect and hardware failure detection for more info"
551 default_value: "AUTO"
553 - name: mag_declination
554 description: "Current location magnetic declination in format. For example, -6deg 37min = -637 for Japan. Leading zero in ddd not required. Get your local magnetic declination here: http://magnetic-declination.com/ . Not in use if inav_auto_mag_decl is turned on and you acquire valid GPS fix."
559 description: "Magnetometer calibration X offset. If its 0 none offset has been applied and calibration is failed."
561 field: magZero.raw[X]
565 description: "Magnetometer calibration Y offset. If its 0 none offset has been applied and calibration is failed."
567 field: magZero.raw[Y]
571 description: "Magnetometer calibration Z offset. If its 0 none offset has been applied and calibration is failed."
573 field: magZero.raw[Z]
577 description: "Magnetometer calibration X gain. If 1024, no calibration or calibration failed"
583 description: "Magnetometer calibration Y gain. If 1024, no calibration or calibration failed"
589 description: "Magnetometer calibration Z gain. If 1024, no calibration or calibration failed"
594 - name: mag_calibration_time
595 description: "Adjust how long time the Calibration of mag will last."
597 field: magCalibrationTimeLimit
601 description: "Allow to chose between built-in and external compass sensor if they are connected to separate buses. Currently only for REVO target"
602 condition: USE_DUAL_MAG
606 - name: align_mag_roll
607 description: "Set the external mag alignment on the roll axis (in 0.1 degree steps). If this value is non-zero, the compass is assumed to be externally mounted and both the board and on-board compass alignent (align_mag) are ignored. See also align_mag_pitch and align_mag_yaw."
609 field: rollDeciDegrees
612 - name: align_mag_pitch
613 description: "Same as align_mag_roll, but for the pitch axis."
615 field: pitchDeciDegrees
618 - name: align_mag_yaw
619 description: "Same as align_mag_roll, but for the yaw axis."
621 field: yawDeciDegrees
625 - name: PG_BAROMETER_CONFIG
626 type: barometerConfig_t
627 headers: ["sensors/barometer.h"]
630 - name: baro_hardware
631 description: "Selection of baro hardware. See Wiki Sensor auto detect and hardware failure detection for more info"
632 default_value: "AUTO"
634 - name: baro_cal_tolerance
635 description: "Baro calibration tolerance in cm. The default should allow the noisiest baro to complete calibration [cm]."
637 field: baro_calibration_tolerance
641 - name: PG_PITOTMETER_CONFIG
642 type: pitotmeterConfig_t
643 headers: ["sensors/pitotmeter.h"]
646 - name: pitot_hardware
647 description: "Selection of pitot hardware."
648 default_value: "NONE"
649 table: pitot_hardware
650 - name: pitot_lpf_milli_hz
651 description: "Pitot tube lowpass filter cutoff frequency. Lower cutoff frequencies result in smoother response at expense of command control delay"
656 description: "Pitot tube scale factor"
663 headers: ["rx/rx.h", "rx/spektrum.h"]
665 - name: receiver_type
666 description: "Selection of receiver (RX) type. Additional configuration of a `serialrx_provider` and a UART will be needed for `SERIAL`"
667 default_value: :target
671 description: "These are min/max values (in us) which, when a channel is smaller (min) or larger (max) than the value will activate various RC commands, such as arming, or stick configuration. Normally, every RC channel should be set so that min = 1000us, max = 2000us. On most transmitters this usually means 125% endpoints. Default check values are 100us above/below this value."
677 description: "These are min/max values (in us) which, when a channel is smaller (min) or larger (max) than the value will activate various RC commands, such as arming, or stick configuration. Normally, every RC channel should be set so that min = 1000us, max = 2000us. On most transmitters this usually means 125% endpoints. Default check values are 100us above/below this value."
683 description: "Source of RSSI input. Possible values: `NONE`, `AUTO`, `ADC`, `CHANNEL`, `PROTOCOL`, `MSP`"
684 default_value: "AUTO"
688 description: "RX channel containing the RSSI signal"
691 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
693 description: "The minimum RSSI value sent by the receiver, in %. For example, if your receiver's minimum RSSI value shows as 42% in the configurator/OSD set this parameter to 42. See also rssi_max. Note that rssi_min can be set to a value bigger than rssi_max to invert the RSSI calculation (i.e. bigger values mean lower RSSI)."
696 min: RSSI_VISIBLE_VALUE_MIN
697 max: RSSI_VISIBLE_VALUE_MAX
699 description: "The maximum RSSI value sent by the receiver, in %. For example, if your receiver's maximum RSSI value shows as 83% in the configurator/OSD set this parameter to 83. See also rssi_min."
702 min: RSSI_VISIBLE_VALUE_MIN
703 max: RSSI_VISIBLE_VALUE_MAX
704 - name: sbus_sync_interval
705 field: sbusSyncInterval
706 description: "SBUS sync interval in us. Default value is 3000us. Lower values may cause issues with some receivers."
710 - name: rc_filter_lpf_hz
711 description: "RC data biquad filter cutoff frequency. Lower cutoff frequencies result in smoother response at expense of command control delay. Practical values are 20-50. Set to zero to disable entirely and use unsmoothed RC stick values"
713 field: rcFilterFrequency
716 - name: rc_filter_auto
717 description: "When enabled, INAV will set RC filtering based on refresh rate and smoothing factor."
721 - name: rc_filter_smoothing_factor
722 description: "The RC filter smoothing factor. The higher the value, the more smoothing but also the more delay in response. Value 1 sets the filter at half the refresh rate. Value 100 sets the filter to aprox. 10% of the RC refresh rate"
723 field: autoSmoothFactor
727 - name: serialrx_provider
728 description: "When feature SERIALRX is enabled, this allows connection to several receivers which output data via digital interface resembling serial. See RX section."
729 default_value: :target
730 condition: USE_SERIAL_RX
732 - name: serialrx_inverted
733 description: "Reverse the serial inversion of the serial RX protocol. When this value is OFF, each protocol will use its default signal (e.g. SBUS will use an inverted signal). Some OpenLRS receivers produce a non-inverted SBUS signal. This setting supports this type of receivers (including modified FrSKY)."
735 condition: USE_SERIAL_RX
737 - name: spektrum_sat_bind
738 description: "0 = disabled. Used to bind the spektrum satellite to RX"
739 condition: USE_SPEKTRUM_BIND
740 min: SPEKTRUM_SAT_BIND_DISABLED
741 max: SPEKTRUM_SAT_BIND_MAX
742 default_value: :SPEKTRUM_SAT_BIND_DISABLED
743 - name: srxl2_unit_id
744 condition: USE_SERIALRX_SRXL2
748 - name: srxl2_baud_fast
749 condition: USE_SERIALRX_SRXL2
753 description: "Defines the shortest pulse width value used when ensuring the channel value is valid. If the receiver gives a pulse value lower than this value then the channel will be marked as bad and will default to the value of mid_rc."
758 description: "Defines the longest pulse width value used when ensuring the channel value is valid. If the receiver gives a pulse value higher than this value then the channel will be marked as bad and will default to the value of mid_rc."
762 - name: serialrx_halfduplex
763 description: "Allow serial receiver to operate on UART TX pin. With some receivers will allow control and telemetry over a single wire."
764 default_value: "AUTO"
767 - name: msp_override_channels
768 description: "Mask of RX channels that may be overridden by MSP `SET_RAW_RC`. Note that this requires custom firmware with `USE_RX_MSP` and `USE_MSP_RC_OVERRIDE` compile options and the `MSP RC Override` flight mode."
770 field: mspOverrideChannels
771 condition: USE_MSP_RC_OVERRIDE
775 - name: PG_BLACKBOX_CONFIG
776 type: blackboxConfig_t
777 headers: ["blackbox/blackbox.h"]
778 condition: USE_BLACKBOX
780 - name: blackbox_rate_num
781 description: "Blackbox logging rate numerator. Use num/denom settings to decide if a frame should be logged, allowing control of the portion of logged loop iterations"
786 - name: blackbox_rate_denom
787 description: "Blackbox logging rate denominator. See blackbox_rate_num."
792 - name: blackbox_device
793 description: "Selection of where to write blackbox data"
794 default_value: :target
796 table: blackbox_device
797 - name: sdcard_detect_inverted
798 description: "This setting drives the way SD card is detected in card slot. On some targets (AnyFC F7 clone) different card slot was used and depending of hardware revision ON or OFF setting might be required. If card is not detected, change this value."
799 default_value: :target
800 field: invertedCardDetection
801 condition: USE_SDCARD
804 - name: PG_MOTOR_CONFIG
806 headers: ["flight/mixer.h"]
809 description: "This is the PWM value sent to ESCs when they are not armed. If ESCs beep slowly when powered up, try decreasing this value. It can also be used for calibrating all ESCs at once."
814 - name: motor_pwm_rate
815 description: "Output frequency (in Hz) for motor pins. Applies only to brushed motors. "
820 - name: motor_pwm_protocol
821 description: "Protocol that is used to send motor updates to ESCs. Possible values - STANDARD, ONESHOT125, ONESHOT42, MULTISHOT, DSHOT150, DSHOT300, DSHOT600, DSHOT1200, BRUSHED"
822 default_value: "ONESHOT125"
823 field: motorPwmProtocol
824 table: motor_pwm_protocol
826 field: motorPoleCount
827 description: "The number of motor poles. Required to compute motor RPM"
832 - name: PG_FAILSAFE_CONFIG
833 type: failsafeConfig_t
834 headers: ["flight/failsafe.h"]
836 - name: failsafe_delay
837 description: "Time in deciseconds to wait before activating failsafe when signal is lost. See [Failsafe documentation](Failsafe.md#failsafe_delay)."
841 - name: failsafe_recovery_delay
842 description: "Time in deciseconds to wait before aborting failsafe when signal is recovered. See [Failsafe documentation](Failsafe.md#failsafe_recovery_delay)."
846 - name: failsafe_off_delay
847 description: "Time in deciseconds to wait before turning off motors when failsafe is activated. 0 = No timeout. See [Failsafe documentation](Failsafe.md#failsafe_off_delay)."
851 - name: failsafe_throttle_low_delay
852 description: "If failsafe activated when throttle is low for this much time - bypass failsafe and disarm, in 10th of seconds. 0 = No timeout"
856 - name: failsafe_procedure
857 description: "What failsafe procedure to initiate in Stage 2. See [Failsafe documentation](Failsafe.md#failsafe_throttle)."
858 default_value: "LAND"
859 table: failsafe_procedure
860 - name: failsafe_stick_threshold
861 description: "Threshold for stick motion to consider failsafe condition resolved. If non-zero failsafe won't clear even if RC link is restored - you have to move sticks to exit failsafe."
863 field: failsafe_stick_motion_threshold
866 - name: failsafe_fw_roll_angle
867 description: "Amount of banking when `LAND` (or old `SET-THR`) failsafe is active on a fixed-wing machine. In 1/10 deg (deci-degrees). Negative values = left roll"
871 - name: failsafe_fw_pitch_angle
872 description: "Amount of dive/climb when `LAND` (or old `SET-THR`) failsafe is active on a fixed-wing machine. In 1/10 deg (deci-degrees). Negative values = climb"
876 - name: failsafe_fw_yaw_rate
877 description: "Requested yaw rate to execute when `LAND` (or old `SET-THR`) failsafe is active on a fixed-wing machine. In deg/s. Negative values = left turn"
881 - name: failsafe_min_distance
882 description: "If failsafe happens when craft is closer than this distance in centimeters from home, failsafe will not execute regular failsafe_procedure, but will execute procedure specified in failsafe_min_distance_procedure instead. 0 = Normal failsafe_procedure always taken."
886 - name: failsafe_min_distance_procedure
887 description: "What failsafe procedure to initiate in Stage 2 when craft is closer to home than failsafe_min_distance. See [Failsafe documentation](Failsafe.md#failsafe_throttle)."
888 default_value: "DROP"
889 table: failsafe_procedure
890 - name: failsafe_mission_delay
891 description: "Applies if failsafe occurs when a WP mission is in progress. Sets the time delay in seconds between failsafe occurring and the selected failsafe procedure activating. If set to -1 the failsafe procedure won't activate at all and the mission will continue until the end."
895 - name: failsafe_gps_fix_estimation_delay
896 description: "Controls whether waypoint mission is allowed to proceed with gps fix estimation. Sets the time delay in seconds between gps fix lost event and RTH activation. Minimum delay is 7 seconds. If set to -1 the mission will continue until the end. With default setting(7), waypoint mission is aborted and switched to RTH with 7 seconds delay. RTH is done with GPS Fix estimation."
897 condition: USE_GPS_FIX_ESTIMATION
902 - name: PG_LIGHTS_CONFIG
904 headers: ["io/lights.h"]
905 condition: USE_LIGHTS
907 - name: failsafe_lights
908 description: "Enable or disable the lights when the `FAILSAFE` flight mode is enabled. The target needs to be compiled with `USE_LIGHTS` [ON/OFF]."
910 field: failsafe.enabled
912 - name: failsafe_lights_flash_period
913 description: "Time in milliseconds between two flashes when `failsafe_lights` is ON and `FAILSAFE` flight mode is enabled [40-65535]."
915 field: failsafe.flash_period
918 - name: failsafe_lights_flash_on_time
919 description: "Flash lights ON time in milliseconds when `failsafe_lights` is ON and `FAILSAFE` flight mode is enabled. [20-65535]."
921 field: failsafe.flash_on_time
925 - name: PG_BOARD_ALIGNMENT
926 type: boardAlignment_t
927 headers: ["sensors/boardalignment.h"]
929 - name: align_board_roll
930 description: "Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc"
932 field: rollDeciDegrees
935 - name: align_board_pitch
936 description: "Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc"
938 field: pitchDeciDegrees
941 - name: align_board_yaw
942 description: "Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc"
944 field: yawDeciDegrees
948 - name: PG_BATTERY_METERS_CONFIG
949 type: batteryMetersConfig_t
950 headers: ["sensors/battery_config_structs.h"]
952 - name: vbat_meter_type
953 description: "Vbat voltage source. Possible values: `NONE`, `ADC`, `ESC`. `ESC` required ESC telemetry enebled and running"
957 table: voltage_sensor
960 description: "Battery voltage calibration value. 1100 = 11:1 voltage divider (10k:1k) x 100. Adjust this slightly if reported pack voltage is different from multimeter reading. You can get current voltage by typing \"status\" in cli."
961 default_value: :target
966 - name: battery_capacity_unit
967 description: "Unit used for `battery_capacity`, `battery_capacity_warning` and `battery_capacity_critical` [MAH/MWH] (milliAmpere hour / milliWatt hour)."
970 table: bat_capacity_unit
972 - name: current_meter_scale
973 description: "This sets the output voltage to current scaling for the current sensor in 0.1 mV/A steps. 400 is 40mV/A such as the ACS756 sensor outputs. 183 is the setting for the uberdistro with a 0.25mOhm shunt."
974 default_value: :target
978 - name: current_meter_offset
979 description: "This sets the output offset voltage of the current sensor in millivolts."
980 default_value: :target
981 field: current.offset
984 - name: current_meter_type
985 description: "ADC , VIRTUAL, NONE. The virtual current sensor, once calibrated, estimates the current value from throttle position."
988 table: current_sensor
990 - name: bat_voltage_src
991 description: "Chose between raw and sag compensated battery voltage to use for battery alarms and telemetry. Possible values are `RAW` and `SAG_COMP`"
994 table: bat_voltage_source
997 description: "Power draw at cruise throttle used for remaining flight time/distance estimation in 0.01W unit"
1003 description: "Power draw at zero throttle used for remaining flight time/distance estimation in 0.01W unit"
1008 - name: rth_energy_margin
1009 description: "Energy margin wanted after getting home (percent of battery energy capacity). Use for the remaining flight time/distance calculation"
1013 - name: thr_comp_weight
1014 description: "Weight used for the throttle compensation based on battery voltage. See the [battery documentation](Battery.md#automatic-throttle-compensation-based-on-battery-voltage)"
1016 field: throttle_compensation_weight
1020 - name: PG_BATTERY_PROFILES
1021 type: batteryProfile_t
1022 headers: ["sensors/battery_config_structs.h"]
1023 value_type: BATTERY_CONFIG_VALUE
1026 description: "Number of cells of the battery (0 = auto-detect), see battery documentation. 7S, 9S and 11S batteries cannot be auto-detected."
1032 - name: vbat_cell_detect_voltage
1033 description: "Maximum voltage per cell, used for auto-detecting the number of cells of the battery in 0.01V units."
1035 field: voltage.cellDetect
1039 - name: vbat_max_cell_voltage
1040 description: "Maximum voltage per cell in 0.01V units, default is 4.20V"
1042 field: voltage.cellMax
1046 - name: vbat_min_cell_voltage
1047 description: "Minimum voltage per cell, this triggers battery out alarms, in 0.01V units, default is 330 (3.3V)"
1049 field: voltage.cellMin
1053 - name: vbat_warning_cell_voltage
1054 description: "Warning voltage per cell, this triggers battery-warning alarms, in 0.01V units, default is 350 (3.5V)"
1056 field: voltage.cellWarning
1060 - name: battery_capacity
1061 description: "Set the battery capacity in mAh or mWh (see `battery_capacity_unit`). Used to calculate the remaining battery capacity."
1063 field: capacity.value
1066 - name: battery_capacity_warning
1067 description: "If the remaining battery capacity goes below this threshold the beeper will emit short beeps and the relevant OSD items will blink."
1069 field: capacity.warning
1072 - name: battery_capacity_critical
1073 description: "If the remaining battery capacity goes below this threshold the battery is considered empty and the beeper will emit long beeps."
1075 field: capacity.critical
1078 - name: controlrate_profile
1079 description: "Control rate profile to switch to when the battery profile is selected, 0 to disable and keep the currently selected control rate profile"
1081 field: controlRateProfile
1083 max: MAX_CONTROL_RATE_PROFILE_COUNT
1085 - name: throttle_scale
1086 description: "Throttle scaling factor. `1` means no throttle scaling. `0.5` means throttle scaled down by 50%"
1088 field: motor.throttleScale
1091 - name: throttle_idle
1092 description: "The percentage of the throttle range (`max_throttle` - `min_command`) above `min_command` used for minimum / idle throttle."
1094 field: motor.throttleIdle
1097 - name: turtle_mode_power_factor
1098 field: motor.turtleModePowerFactor
1100 description: "Turtle mode power factor"
1101 condition: USE_DSHOT
1104 - name: failsafe_throttle
1105 description: "Throttle level used for landing when failsafe is enabled. See [Failsafe documentation](Failsafe.md#failsafe_throttle)."
1109 - name: nav_mc_hover_thr
1110 description: "Multicopter hover throttle hint for altitude controller. Should be set to approximate throttle value when drone is hovering."
1112 field: nav.mc.hover_throttle
1115 - name: nav_fw_cruise_thr
1116 description: "Cruise throttle in GPS assisted modes, this includes RTH. Should be set high enough to avoid stalling. This values gives INAV a base for throttle when flying straight, and it will increase or decrease throttle based on pitch of airplane and the parameters below. In addition it will increase throttle if GPS speed gets below 7m/s ( hardcoded )"
1118 field: nav.fw.cruise_throttle
1121 - name: nav_fw_min_thr
1122 description: "Minimum throttle for flying wing in GPS assisted modes"
1124 field: nav.fw.min_throttle
1127 - name: nav_fw_max_thr
1128 description: "Maximum throttle for flying wing in GPS assisted modes"
1130 field: nav.fw.max_throttle
1133 - name: nav_fw_pitch2thr
1134 description: "Amount of throttle applied related to pitch attitude in GPS assisted modes. Throttle = nav_fw_cruise_throttle - (nav_fw_pitch2thr * pitch_angle). (notice that pitch_angle is in degrees and is negative when climbing and positive when diving, and throttle value is constrained between nav_fw_min_thr and nav_fw_max_thr)"
1136 field: nav.fw.pitch_to_throttle
1139 - name: nav_fw_launch_thr
1140 description: "Launch throttle - throttle to be set during launch sequence (pwm units)"
1142 field: nav.fw.launch_throttle
1145 - name: nav_fw_launch_idle_thr
1146 description: "Launch idle throttle - throttle to be set before launch sequence is initiated. If set below minimum throttle it will force motor stop or at idle throttle (depending if the MOTOR_STOP is enabled). If set above minimum throttle it will force throttle to this value (if MOTOR_STOP is enabled it will be handled according to throttle stick position)"
1148 field: nav.fw.launch_idle_throttle
1151 - name: limit_cont_current
1152 description: "Continous current limit (dA), set to 0 to disable"
1153 condition: USE_POWER_LIMITS
1155 field: powerLimits.continuousCurrent
1157 - name: limit_burst_current
1158 description: "Burst current limit (dA): the current which is allowed during `limit_burst_current_time` after which `limit_cont_current` will be enforced, set to 0 to disable"
1159 condition: USE_POWER_LIMITS
1161 field: powerLimits.burstCurrent
1163 - name: limit_burst_current_time
1164 description: "Allowed current burst time (ds) during which `limit_burst_current` is allowed and after which `limit_cont_current` will be enforced"
1165 condition: USE_POWER_LIMITS
1167 field: powerLimits.burstCurrentTime
1169 - name: limit_burst_current_falldown_time
1170 description: "Time slice at the end of the burst time during which the current limit will be ramped down from `limit_burst_current` back down to `limit_cont_current`"
1171 condition: USE_POWER_LIMITS
1173 field: powerLimits.burstCurrentFalldownTime
1175 - name: limit_cont_power
1176 description: "Continous power limit (dW), set to 0 to disable"
1177 condition: USE_POWER_LIMITS && USE_ADC
1179 field: powerLimits.continuousPower
1181 - name: limit_burst_power
1182 description: "Burst power limit (dW): the current which is allowed during `limit_burst_power_time` after which `limit_cont_power` will be enforced, set to 0 to disable"
1183 condition: USE_POWER_LIMITS && USE_ADC
1185 field: powerLimits.burstPower
1187 - name: limit_burst_power_time
1188 description: "Allowed power burst time (ds) during which `limit_burst_power` is allowed and after which `limit_cont_power` will be enforced"
1189 condition: USE_POWER_LIMITS && USE_ADC
1191 field: powerLimits.burstPowerTime
1193 - name: limit_burst_power_falldown_time
1194 description: "Time slice at the end of the burst time during which the power limit will be ramped down from `limit_burst_power` back down to `limit_cont_power`"
1195 condition: USE_POWER_LIMITS && USE_ADC
1197 field: powerLimits.burstPowerFalldownTime
1200 - name: PG_MIXER_PROFILE
1201 type: mixerProfile_t
1202 headers: ["flight/mixer_profile.h"]
1203 value_type: MIXER_CONFIG_VALUE
1205 - name: motor_direction_inverted
1206 description: "Use if you need to inverse yaw motor direction."
1208 field: mixer_config.motorDirectionInverted
1210 - name: platform_type
1211 description: "Defines UAV platform type. Allowed values: \"MULTIROTOR\", \"AIRPLANE\", \"HELICOPTER\", \"TRICOPTER\", \"ROVER\", \"BOAT\". Currently only MULTIROTOR, AIRPLANE and TRICOPTER types are implemented"
1212 default_value: "MULTIROTOR"
1213 field: mixer_config.platformType
1215 table: platform_type
1217 description: "Defines is UAV is capable of having flaps. If ON and AIRPLANE `platform_type` is used, **FLAPERON** flight mode will be available for the pilot"
1219 field: mixer_config.hasFlaps
1221 - name: model_preview_type
1222 description: "ID of mixer preset applied in a Configurator. **Do not modify manually**. Used only for backup/restore reasons."
1224 field: mixer_config.appliedMixerPreset
1227 - name: motorstop_on_low
1228 description: "If enabled, motor will stop when throttle is low on this mixer_profile"
1230 field: mixer_config.motorstopOnLow
1232 - name: mixer_pid_profile_linking
1233 description: "If enabled, pid profile_index will follow mixer_profile index. Set to OFF(default) if you want to handle PID profile by your self. Recommend to set to ON on all mixer_profiles to let the mixer_profile handle the PID profile switching on a VTOL or mixed platform type setup."
1235 field: mixer_config.PIDProfileLinking
1237 - name: mixer_automated_switch
1238 description: "If set to on, This mixer_profile will try to switch to another mixer_profile when 1.RTH heading home is requested and distance to home is lager than 3*nav_fw_loiter_radius on mixer_profile is a MULTIROTOR or TRICOPTER platform_type. 2. RTH landing is requested on this mixer_profile is a AIRPLANE platform_type"
1240 field: mixer_config.automated_switch
1242 - name: mixer_switch_trans_timer
1243 description: "If switch another mixer_profile is scheduled by mixer_automated_switch or mixer_automated_switch. Activate Mixertransion motor/servo mixing for this many decisecond(0.1s) before the actual mixer_profile switch."
1245 field: mixer_config.switchTransitionTimer
1248 - name: tailsitter_orientation_offset
1249 description: "Apply a 90 deg pitch offset in sensor aliment for tailsitter flying mode"
1251 field: mixer_config.tailsitterOrientationOffset
1254 - name: PG_REVERSIBLE_MOTORS_CONFIG
1255 type: reversibleMotorsConfig_t
1257 - name: 3d_deadband_low
1258 description: "Low value of throttle deadband for 3D mode (when stick is in the 3d_deadband_throttle range, the fixed values of 3d_deadband_low / _high are used instead)"
1263 - name: 3d_deadband_high
1264 description: "High value of throttle deadband for 3D mode (when stick is in the deadband range, the value in 3d_neutral is used instead)"
1266 field: deadband_high
1270 description: "Neutral (stop) throttle value for 3D mode"
1276 - name: PG_SERVO_CONFIG
1278 headers: ["flight/servos.h"]
1280 - name: servo_protocol
1281 description: "An option to chose the protocol/option that would be used to output servo data. Possible options `PWM` (FC servo outputs), `SBUS` (S.Bus protocol output via a configured serial port)"
1282 default_value: "PWM"
1283 field: servo_protocol
1284 table: servo_protocol
1285 - name: servo_center_pulse
1286 description: "Servo midpoint"
1288 field: servoCenterPulse
1291 - name: servo_pwm_rate
1292 description: "Output frequency (in Hz) servo pins. When using tricopters or gimbal with digital servo, this rate can be increased. Max of 498Hz (for 500Hz pwm period), and min of 50Hz. Most digital servos will support for example 330Hz."
1297 - name: servo_lpf_hz
1298 description: "Selects the servo PWM output cutoff frequency. Value is in [Hz]"
1300 field: servo_lowpass_freq
1303 - name: flaperon_throw_offset
1304 description: "Defines throw range in us for both ailerons that will be passed to servo mixer via input source 14 (`FEATURE FLAPS`) when FLAPERON mode is activated."
1306 min: FLAPERON_THROW_MIN
1307 max: FLAPERON_THROW_MAX
1308 - name: tri_unarmed_servo
1309 description: "On tricopter mix only, if this is set to ON, servo will always be correcting regardless of armed state. to disable this, set it to OFF."
1312 - name: servo_autotrim_rotation_limit
1313 description: "Servo midpoints are only updated when total aircraft rotation is less than this threshold [deg/s]. Only applies when using `feature FW_AUTOTRIM`."
1318 - name: PG_CONTROL_RATE_PROFILES
1319 type: controlRateConfig_t
1320 headers: ["fc/controlrate_profile_config_struct.h"]
1321 value_type: CONTROL_RATE_VALUE
1324 description: "Throttle value when the stick is set to mid-position. Used in the throttle curve calculation."
1326 field: throttle.rcMid8
1330 description: "Throttle exposition value"
1332 field: throttle.rcExpo8
1336 description: "Throttle PID attenuation reduces influence of PDFF on ROLL and PITCH of multi-rotor, PIDFF on ROLL,PITCH,YAW OF fixed_wing as throttle increases. For every 1% throttle after the TPA breakpoint, P is reduced by the TPA rate."
1338 field: throttle.dynPID
1341 - name: tpa_breakpoint
1342 description: "See tpa_rate."
1344 field: throttle.pa_breakpoint
1348 description: "Throttle PID attenuation also reduces influence on YAW for multi-rotor, Should be set to ON for tilting rotors."
1350 field: throttle.dynPID_on_YAW
1352 - name: fw_tpa_time_constant
1353 description: "TPA smoothing and delay time constant to reflect non-instant speed/throttle response of the plane. See **PID Attenuation and scaling** Wiki for full details."
1355 field: throttle.fixedWingTauMs
1359 description: "Exposition value used for the PITCH/ROLL axes by all the stabilized flights modes (all but `MANUAL`)"
1361 field: stabilized.rcExpo8
1365 description: "Exposition value used for the YAW axis by all the stabilized flights modes (all but `MANUAL`)"
1367 field: stabilized.rcYawExpo8
1370 # New rates are in dps/10. That means, Rate of 20 means 200dps of rotation speed on given axis.
1371 # Rate 180 (1800dps) is max. value gyro can measure reliably
1373 description: "Defines rotation rate on ROLL axis that UAV will try to archive on max. stick deflection. Rates are defined in tens of degrees (deca-degrees) per second [rate = dps/10]. That means, rate 20 represents 200dps rotation speed. Default 20 (200dps) is more less equivalent of old Cleanflight/Baseflight rate 0. Max. 180 (1800dps) is what gyro can measure."
1375 field: stabilized.rates[FD_ROLL]
1376 min: ROLL_PITCH_RATE_MIN
1377 max: ROLL_PITCH_RATE_MAX
1379 description: "Defines rotation rate on PITCH axis that UAV will try to archive on max. stick deflection. Rates are defined in tens of degrees (deca-degrees) per second [rate = dps/10]. That means, rate 20 represents 200dps rotation speed. Default 20 (200dps) is more less equivalent of old Cleanflight/Baseflight rate 0. Max. 180 (1800dps) is what gyro can measure."
1381 field: stabilized.rates[FD_PITCH]
1382 min: ROLL_PITCH_RATE_MIN
1383 max: ROLL_PITCH_RATE_MAX
1385 description: "Defines rotation rate on YAW axis that UAV will try to archive on max. stick deflection. Rates are defined in tens of degrees (deca-degrees) per second [rate = dps/10]. That means, rate 20 represents 200dps rotation speed. Default 20 (200dps) is more less equivalent of old Cleanflight/Baseflight rate 0. Max. 180 (1800dps) is what gyro can measure."
1387 field: stabilized.rates[FD_YAW]
1390 - name: manual_rc_expo
1391 description: "Exposition value used for the PITCH/ROLL axes by the `MANUAL` flight mode [0-100]"
1393 field: manual.rcExpo8
1396 - name: manual_rc_yaw_expo
1397 description: "Exposition value used for the YAW axis by the `MANUAL` flight mode [0-100]"
1399 field: manual.rcYawExpo8
1402 - name: manual_roll_rate
1403 description: "Servo travel multiplier for the ROLL axis in `MANUAL` flight mode [0-100]%"
1405 field: manual.rates[FD_ROLL]
1406 min: MANUAL_RATE_MIN
1407 max: MANUAL_RATE_MAX
1408 - name: manual_pitch_rate
1409 description: "Servo travel multiplier for the PITCH axis in `MANUAL` flight mode [0-100]%"
1411 field: manual.rates[FD_PITCH]
1412 min: MANUAL_RATE_MIN
1413 max: MANUAL_RATE_MAX
1414 - name: manual_yaw_rate
1415 description: "Servo travel multiplier for the YAW axis in `MANUAL` flight mode [0-100]%"
1417 field: manual.rates[FD_YAW]
1418 min: MANUAL_RATE_MIN
1419 max: MANUAL_RATE_MAX
1420 - name: fpv_mix_degrees
1421 description: "The tilt angle of the FPV camera in degrees, used by the FPV ANGLE MIX mode"
1422 field: misc.fpvCamAngleDegrees
1426 - name: rate_dynamics_center_sensitivity
1427 field: rateDynamics.sensitivityCenter
1431 description: "The center stick sensitivity for Rate Dynamics"
1432 condition: USE_RATE_DYNAMICS
1433 - name: rate_dynamics_end_sensitivity
1434 field: rateDynamics.sensitivityEnd
1438 description: "The end stick sensitivity for Rate Dynamics"
1439 condition: USE_RATE_DYNAMICS
1440 - name: rate_dynamics_center_correction
1441 field: rateDynamics.correctionCenter
1445 description: "The center stick correction for Rate Dynamics"
1446 condition: USE_RATE_DYNAMICS
1447 - name: rate_dynamics_end_correction
1448 field: rateDynamics.correctionEnd
1452 description: "The end stick correction for Rate Dynamics"
1453 condition: USE_RATE_DYNAMICS
1454 - name: rate_dynamics_center_weight
1455 field: rateDynamics.weightCenter
1459 description: "The center stick weight for Rate Dynamics"
1460 condition: USE_RATE_DYNAMICS
1461 - name: rate_dynamics_end_weight
1462 field: rateDynamics.weightEnd
1466 description: "The end stick weight for Rate Dynamics"
1467 condition: USE_RATE_DYNAMICS
1469 - name: PG_SERIAL_CONFIG
1470 type: serialConfig_t
1471 headers: ["io/serial.h"]
1473 - name: reboot_character
1474 description: "Special character used to trigger reboot"
1479 - name: PG_IMU_CONFIG
1481 headers: ["flight/imu.h"]
1484 description: "Inertial Measurement Unit KP Gain for accelerometer measurements"
1489 description: "Inertial Measurement Unit KI Gain for accelerometer measurements"
1493 - name: ahrs_dcm_kp_mag
1494 description: "Inertial Measurement Unit KP Gain for compass measurements"
1498 - name: ahrs_dcm_ki_mag
1499 description: "Inertial Measurement Unit KI Gain for compass measurements"
1504 description: "If the aircraft tilt angle exceed this value the copter will refuse to arm."
1508 - name: ahrs_acc_ignore_rate
1509 description: "Total gyro rotation rate threshold [deg/s] before scaling to consider accelerometer trustworthy"
1511 field: acc_ignore_rate
1514 - name: ahrs_acc_ignore_slope
1515 description: "Half-width of the interval to gradually reduce accelerometer weight. Centered at `imu_acc_ignore_rate` (exactly 50% weight)"
1517 field: acc_ignore_slope
1520 - name: ahrs_gps_yaw_windcomp
1521 description: "Wind compensation in heading estimation from gps groundcourse(fixed wing only)"
1523 field: gps_yaw_windcomp
1525 - name: ahrs_inertia_comp_method
1526 description: "Inertia force compensation method when gps is avaliable, VELNED use the accleration from gps, TURNRATE calculates accleration by turnrate multiplied by speed, ADAPTIVE choose best result from two in each ahrs loop"
1527 default_value: ADAPTIVE
1528 field: inertia_comp_method
1529 table: imu_inertia_comp_method
1530 - name: ahrs_gps_yaw_weight
1531 description: "Arhs gps yaw weight when mag is avaliable, 0 means no gps yaw, 100 means equal weight as compass"
1533 field: gps_yaw_weight
1537 - name: PG_ARMING_CONFIG
1538 type: armingConfig_t
1540 - name: fixed_wing_auto_arm
1541 description: "Auto-arm fixed wing aircraft on throttle above min_check, and disarming with stick commands are disabled, so power cycle is required to disarm. Requires enabled motorstop and no arm switch configured."
1544 - name: disarm_always
1545 description: "Disarms the motors independently of throttle value. Setting to OFF reverts to the old behaviour of disarming only when the throttle is low."
1548 - name: switch_disarm_delay
1549 description: "Delay before disarming when requested by switch (ms) [0-1000]"
1551 field: switchDisarmDelayMs
1554 - name: prearm_timeout
1555 description: "Duration (ms) for which Prearm being activated is valid. after this, Prearm needs to be reset. 0 means Prearm does not timeout."
1556 default_value: 10000
1557 field: prearmTimeoutMs
1561 - name: PG_GENERAL_SETTINGS
1562 headers: ["config/general_settings.h"]
1563 type: generalSettings_t
1565 - name: applied_defaults
1566 description: "Internal (configurator) hint. Should not be changed manually"
1568 field: appliedDefaults
1574 headers: ["flight/ez_tune.h"]
1575 type: ezTuneSettings_t
1576 value_type: EZ_TUNE_VALUE
1579 description: "Enables EzTune feature"
1583 - name: ez_filter_hz
1584 description: "EzTune filter cutoff frequency"
1589 - name: ez_axis_ratio
1590 description: "EzTune axis ratio"
1596 description: "EzTune response"
1602 description: "EzTune damping"
1607 - name: ez_stability
1608 description: "EzTune stability"
1613 - name: ez_aggressiveness
1614 description: "EzTune aggressiveness"
1616 field: aggressiveness
1620 description: "EzTune rate"
1626 description: "EzTune expo"
1631 - name: ez_snappiness
1632 description: "EzTune snappiness"
1638 - name: PG_RPM_FILTER_CONFIG
1639 headers: ["flight/rpm_filter.h"]
1640 condition: USE_RPM_FILTER
1641 type: rpmFilterConfig_t
1643 - name: rpm_gyro_filter_enabled
1644 description: "Enables gyro RPM filtere. Set to `ON` only when ESC telemetry is working and rotation speed of the motors is correctly reported to INAV"
1646 field: gyro_filter_enabled
1648 - name: rpm_gyro_harmonics
1649 description: "Number of harmonic frequences to be covered by gyro RPM filter. Default value of `1` usually works just fine"
1651 field: gyro_harmonics
1655 - name: rpm_gyro_min_hz
1656 description: "The lowest frequency for gyro RPM filtere. Default `150` is fine for 5\" mini-quads. On 7-inch drones you can lower even down to `60`-`70`"
1663 description: "Q factor for gyro RPM filter. Lower values give softer, wider attenuation. Usually there is no need to change this setting"
1669 - name: PG_GPS_CONFIG
1670 headers: [ "io/gps.h" ]
1674 - name: gps_provider
1675 description: "Which GPS protocol to be used."
1676 default_value: "UBLOX"
1680 - name: gps_sbas_mode
1681 description: "Which SBAS mode to be used"
1682 default_value: "NONE"
1684 table: gps_sbas_mode
1686 - name: gps_dyn_model
1687 description: "GPS navigation model: Pedestrian, Automotive, Air<1g, Air<2g, Air<4g. Default is AIR_2G. Use pedestrian/Automotive with caution, can cause flyaways with fast flying."
1688 default_value: "AIR_2G"
1690 table: gps_dyn_model
1692 - name: gps_auto_config
1693 description: "Enable automatic configuration of UBlox GPS receivers."
1697 - name: gps_auto_baud
1698 description: "Automatic configuration of GPS baudrate(The specified baudrate in configured in ports will be used) when used with UBLOX GPS"
1702 - name: gps_auto_baud_max_supported
1703 description: "Max baudrate supported by GPS unit. This is used during autobaud. M8 supports up to 460400, M10 supports up to 921600 and 230400 is the value used before INAV 7.0"
1704 default_value: "230400"
1705 table: gps_auto_baud_max
1708 - name: gps_ublox_use_galileo
1709 description: "Enable use of Galileo satellites. This is at the expense of other regional constellations, so benefit may also be regional. Requires M8N and Ublox firmware 3.x (or later) [OFF/ON]."
1711 field: ubloxUseGalileo
1713 - name: gps_ublox_use_beidou
1714 description: "Enable use of Beidou satellites. This is at the expense of other regional constellations, so benefit may also be regional. Requires gps hardware support [OFF/ON]."
1716 field: ubloxUseBeidou
1718 - name: gps_ublox_use_glonass
1719 description: "Enable use of Glonass satellites. This is at the expense of other regional constellations, so benefit may also be regional. Requires gps haardware support [OFF/ON]."
1721 field: ubloxUseGlonass
1723 - name: gps_min_sats
1724 description: "Minimum number of GPS satellites in view to acquire GPS_FIX and consider GPS position valid. Some GPS receivers appeared to be very inaccurate with low satellite count."
1729 - name: gps_ublox_nav_hz
1730 description: "Navigation update rate for UBLOX receivers. Some receivers may limit the maximum number of satellites tracked when set to a higher rate or even stop sending navigation updates if the value is too high. Some M10 devices can do up to 25Hz. 10 is a safe value for M8 and newer."
1738 - name: PG_RC_CONTROLS_CONFIG
1739 type: rcControlsConfig_t
1740 headers: ["fc/rc_controls.h"]
1743 description: "These are values (in us) by how much RC input can be different before it's considered valid. For transmitters with jitter on outputs, this value can be increased. Defaults are zero, but can be increased up to 10 or so if rc inputs twitch while idle."
1747 - name: yaw_deadband
1748 description: "These are values (in us) by how much RC input can be different before it's considered valid. For transmitters with jitter on outputs, this value can be increased. Defaults are zero, but can be increased up to 10 or so if rc inputs twitch while idle."
1752 - name: pos_hold_deadband
1753 description: "Stick deadband in [r/c points], applied after r/c deadband and expo. Used for adjustments in navigation modes."
1757 - name: alt_hold_deadband
1758 description: "Defines the deadband of throttle during alt_hold [r/c points]"
1762 - name: 3d_deadband_throttle
1763 description: "Throttle signal will be held to a fixed value when throttle is centered with an error margin defined in this parameter."
1765 field: mid_throttle_deadband
1768 - name: airmode_type
1769 description: "Defines the Airmode state handling type. Default **STICK_CENTER** is the classical approach in which Airmode is always active if enabled, but when the throttle is low and ROLL/PITCH/YAW sticks are centered, Iterms is not allowed to grow (ANTI_WINDUP). **THROTTLE_THRESHOLD** is the Airmode behavior known from Betaflight. In this mode, Airmode is active as soon THROTTLE position is above `airmode_throttle_threshold` and stays active until disarm. ANTI_WINDUP is never triggered. For small Multirotors (up to 7-inch propellers) it is suggested to switch to **THROTTLE_THRESHOLD** since it keeps full stabilization no matter what pilot does with the sticks. Fixed Wings always use **STICK_CENTER_ONCE** or **STICK_CENTER** modes."
1770 default_value: "STICK_CENTER"
1771 field: airmodeHandlingType
1772 table: airmodeHandlingType
1773 - name: airmode_throttle_threshold
1774 description: "Defines airmode THROTTLE activation threshold when `airmode_type` **THROTTLE_THRESHOLD** is used"
1776 field: airmodeThrottleThreshold
1780 - name: PG_PID_PROFILE
1782 headers: ["flight/pid.h"]
1783 value_type: PROFILE_VALUE
1786 description: "Multicopter rate stabilisation P-gain for PITCH"
1788 field: bank_mc.pid[PID_PITCH].P
1792 description: "Multicopter rate stabilisation I-gain for PITCH"
1794 field: bank_mc.pid[PID_PITCH].I
1798 description: "Multicopter rate stabilisation D-gain for PITCH"
1800 field: bank_mc.pid[PID_PITCH].D
1804 description: "Multicopter Control Derivative gain for PITCH (known as 'Feed Forward' in Betaflight). The CD intoduces a term to the PID controller that is the magnitude of the Setpoint change. Fast inputs produce a high CD gain to help push the MC into a move; in advance of the P-gain if set high enough."
1806 field: bank_mc.pid[PID_PITCH].FF
1810 description: "Multicopter rate stabilisation P-gain for ROLL"
1812 field: bank_mc.pid[PID_ROLL].P
1816 description: "Multicopter rate stabilisation I-gain for ROLL"
1818 field: bank_mc.pid[PID_ROLL].I
1822 description: "Multicopter rate stabilisation D-gain for ROLL"
1824 field: bank_mc.pid[PID_ROLL].D
1828 description: "Multicopter Control Derivative gain for ROLL (known as 'Feed Forward' in Betaflight). The CD intoduces a term to the PID controller that is the magnitude of the Setpoint change. Fast inputs produce a high CD gain to help push the MC into a move; in advance of the P-gain if set high enough."
1830 field: bank_mc.pid[PID_ROLL].FF
1834 description: "Multicopter rate stabilisation P-gain for YAW"
1836 field: bank_mc.pid[PID_YAW].P
1840 description: "Multicopter rate stabilisation I-gain for YAW"
1842 field: bank_mc.pid[PID_YAW].I
1846 description: "Multicopter rate stabilisation D-gain for YAW"
1848 field: bank_mc.pid[PID_YAW].D
1852 description: "Multicopter Control Derivative gain for YAW (known as 'Feed Forward' in Betaflight). The CD intoduces a term to the PID controller that is the magnitude of the Setpoint change. Fast inputs produce a high CD gain to help push the MC into a move; in advance of the P-gain if set high enough."
1854 field: bank_mc.pid[PID_YAW].FF
1858 description: "Multicopter attitude stabilisation P-gain"
1860 field: bank_mc.pid[PID_LEVEL].P
1864 description: "Multicopter attitude stabilisation low-pass filter cutoff"
1866 field: bank_mc.pid[PID_LEVEL].I
1870 description: "Multicopter attitude stabilisation HORIZON transition point"
1872 field: bank_mc.pid[PID_LEVEL].D
1876 description: "Fixed-wing rate stabilisation P-gain for PITCH"
1878 field: bank_fw.pid[PID_PITCH].P
1882 description: "Fixed-wing rate stabilisation I-gain for PITCH"
1884 field: bank_fw.pid[PID_PITCH].I
1888 description: "Fixed wing rate stabilisation D-gain for PITCH"
1890 field: bank_fw.pid[PID_PITCH].D
1894 description: "Fixed-wing rate stabilisation FF-gain for PITCH"
1896 field: bank_fw.pid[PID_PITCH].FF
1900 description: "Fixed-wing rate stabilisation P-gain for ROLL"
1902 field: bank_fw.pid[PID_ROLL].P
1906 description: "Fixed-wing rate stabilisation I-gain for ROLL"
1908 field: bank_fw.pid[PID_ROLL].I
1912 description: "Fixed wing rate stabilisation D-gain for ROLL"
1914 field: bank_fw.pid[PID_ROLL].D
1918 description: "Fixed-wing rate stabilisation FF-gain for ROLL"
1920 field: bank_fw.pid[PID_ROLL].FF
1924 description: "Fixed-wing rate stabilisation P-gain for YAW"
1926 field: bank_fw.pid[PID_YAW].P
1930 description: "Fixed-wing rate stabilisation I-gain for YAW"
1932 field: bank_fw.pid[PID_YAW].I
1936 description: "Fixed wing rate stabilisation D-gain for YAW"
1938 field: bank_fw.pid[PID_YAW].D
1942 description: "Fixed-wing rate stabilisation FF-gain for YAW"
1944 field: bank_fw.pid[PID_YAW].FF
1948 description: "Fixed-wing attitude stabilisation P-gain"
1950 field: bank_fw.pid[PID_LEVEL].P
1954 description: "Fixed-wing attitude stabilisation low-pass filter cutoff"
1956 field: bank_fw.pid[PID_LEVEL].I
1960 description: "Fixed-wing attitude stabilisation HORIZON transition point"
1962 field: bank_fw.pid[PID_LEVEL].D
1965 - name: max_angle_inclination_rll
1966 description: "Maximum inclination in level (angle) mode (ROLL axis). 100=10°"
1968 field: max_angle_inclination[FD_ROLL]
1971 - name: max_angle_inclination_pit
1972 description: "Maximum inclination in level (angle) mode (PITCH axis). 100=10°"
1974 field: max_angle_inclination[FD_PITCH]
1977 - name: dterm_lpf_hz
1978 description: "Dterm low pass filter cutoff frequency. Default setting is very conservative and small multirotors should use higher value between 80 and 100Hz. 80 seems like a gold spot for 7-inch builds while 100 should work best with 5-inch machines. If motors are getting too hot, lower the value"
1982 - name: dterm_lpf_type
1983 description: "Defines the type of stage 1 D-term LPF filter. Possible values: `PT1`, `BIQUAD`, `PT2`, `PT3`."
1984 default_value: "PT2"
1985 field: dterm_lpf_type
1986 table: filter_type_full
1988 description: "Yaw P term low pass filter cutoff frequency. Should be disabled (set to `0`) on small multirotors (7 inches and below)"
1992 - name: fw_reference_airspeed
1993 description: "Reference airspeed. Set this to airspeed at which PIDs were tuned. Usually should be set to cruise airspeed. Also used for coordinated turn calculation if airspeed sensor is not present."
1995 field: fixedWingReferenceAirspeed
1998 - name: fw_turn_assist_yaw_gain
1999 description: "Gain required to keep the yaw rate consistent with the turn rate for a coordinated turn (in TURN_ASSIST mode). Value significantly different from 1.0 indicates a problem with the airspeed calibration (if present) or value of `fw_reference_airspeed` parameter"
2001 field: fixedWingCoordinatedYawGain
2004 - name: fw_turn_assist_pitch_gain
2005 description: "Gain required to keep constant pitch angle during coordinated turns (in TURN_ASSIST mode). Value significantly different from 1.0 indicates a problem with the airspeed calibration (if present) or value of `fw_reference_airspeed` parameter"
2007 field: fixedWingCoordinatedPitchGain
2010 - name: fw_yaw_iterm_freeze_bank_angle
2011 description: "Yaw Iterm is frozen when bank angle is above this threshold [degrees]. This solves the problem of the rudder counteracting turns by partially disabling yaw stabilization when making banked turns. Setting to 0 (the default) disables this feature. Only applies when autopilot is not active and TURN ASSIST is disabled."
2013 field: fixedWingYawItermBankFreeze
2016 - name: iterm_windup
2017 description: "Used to prevent Iterm accumulation on during maneuvers. Iterm will be dampened when motors are reaching it's limit (when requested motor correction range is above percentage specified by this parameter)"
2019 field: itermWindupPointPercent
2022 - name: pid_iterm_limit_percent
2023 description: "Limits max/min I-term value in stabilization PID controller. It solves the problem of servo saturation before take-off/throwing the airplane into the air. Or multirotors with low authority. By default, error accumulated in I-term can not exceed 33% of total pid throw (around 165us on deafult pidsum_limit of pitch/roll). Set 0 to disable completely."
2025 field: pidItermLimitPercent
2028 - name: rate_accel_limit_roll_pitch
2029 description: "Limits acceleration of ROLL/PITCH rotation speed that can be requested by stick input. In degrees-per-second-squared. Small and powerful UAV flies great with high acceleration limit ( > 5000 dps^2 and even > 10000 dps^2). Big and heavy multirotors will benefit from low acceleration limit (~ 360 dps^2). When set correctly, it greatly improves stopping performance. Value of 0 disables limiting."
2031 field: axisAccelerationLimitRollPitch
2033 - name: rate_accel_limit_yaw
2034 description: "Limits acceleration of YAW rotation speed that can be requested by stick input. In degrees-per-second-squared. Small and powerful UAV flies great with high acceleration limit ( > 10000 dps^2). Big and heavy multirotors will benefit from low acceleration limit (~ 180 dps^2). When set correctly, it greatly improves stopping performance and general stability during yaw turns. Value of 0 disables limiting."
2035 default_value: 10000
2036 field: axisAccelerationLimitYaw
2038 - name: heading_hold_rate_limit
2039 description: "This setting limits yaw rotation rate that HEADING_HOLD controller can request from PID inner loop controller. It is independent from manual yaw rate and used only when HEADING_HOLD flight mode is enabled by pilot, RTH or WAYPOINT modes."
2040 min: HEADING_HOLD_RATE_LIMIT_MIN
2041 max: HEADING_HOLD_RATE_LIMIT_MAX
2043 - name: nav_mc_pos_z_p
2044 description: "P gain of altitude PID controller (Multirotor)"
2045 field: bank_mc.pid[PID_POS_Z].P
2049 - name: nav_mc_vel_z_p
2050 description: "P gain of velocity PID controller"
2051 field: bank_mc.pid[PID_VEL_Z].P
2055 - name: nav_mc_vel_z_i
2056 description: "I gain of velocity PID controller"
2057 field: bank_mc.pid[PID_VEL_Z].I
2061 - name: nav_mc_vel_z_d
2062 description: "D gain of velocity PID controller"
2063 field: bank_mc.pid[PID_VEL_Z].D
2067 - name: nav_mc_pos_xy_p
2068 description: "Controls how fast the drone will fly towards the target position. This is a multiplier to convert displacement to target velocity"
2069 field: bank_mc.pid[PID_POS_XY].P
2073 - name: nav_mc_vel_xy_p
2074 description: "P gain of Position-Rate (Velocity to Acceleration) PID controller. Higher P means stronger response when position error occurs. Too much P might cause \"nervous\" behavior and oscillations"
2075 field: bank_mc.pid[PID_VEL_XY].P
2079 - name: nav_mc_vel_xy_i
2080 description: "I gain of Position-Rate (Velocity to Acceleration) PID controller. Used for drift compensation (caused by wind for example). Higher I means stronger response to drift. Too much I gain might cause target overshot"
2081 field: bank_mc.pid[PID_VEL_XY].I
2085 - name: nav_mc_vel_xy_d
2086 description: "D gain of Position-Rate (Velocity to Acceleration) PID controller. It can damp P and I. Increasing D might help when drone overshoots target."
2087 field: bank_mc.pid[PID_VEL_XY].D
2091 - name: nav_mc_vel_xy_ff
2092 description: "FF gain of Position-Rate (Velocity to Acceleration)"
2093 field: bank_mc.pid[PID_VEL_XY].FF
2097 - name: nav_mc_heading_p
2098 description: "P gain of Heading Hold controller (Multirotor)"
2100 field: bank_mc.pid[PID_HEADING].P
2103 - name: nav_mc_vel_xy_dterm_lpf_hz
2104 description: "D-term low pass filter cutoff frequency for horizontal velocity PID controller (Multirotor). It allows to smooth the PosHold CRUISE, WP and RTH when Multirotor is traveling at full speed. Dterm is not attenuated at low speeds, breaking and accelerating."
2105 field: navVelXyDTermLpfHz
2109 - name: nav_mc_vel_xy_dterm_attenuation
2110 description: "Maximum D-term attenution percentage for horizontal velocity PID controller (Multirotor). It allows to smooth the PosHold CRUISE, WP and RTH when Multirotor is traveling at full speed. Dterm is not attenuated at low speeds, breaking and accelerating."
2111 field: navVelXyDtermAttenuation
2115 - name: nav_mc_vel_xy_dterm_attenuation_start
2116 description: "A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation begins"
2118 field: navVelXyDtermAttenuationStart
2121 - name: nav_mc_vel_xy_dterm_attenuation_end
2122 description: "A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation reaches maximum"
2124 field: navVelXyDtermAttenuationEnd
2127 - name: nav_fw_pos_z_p
2128 description: "P gain of altitude PID controller (Fixedwing)"
2130 field: bank_fw.pid[PID_POS_Z].P
2133 - name: nav_fw_pos_z_i
2134 description: "I gain of altitude PID controller (Fixedwing)"
2136 field: bank_fw.pid[PID_POS_Z].I
2139 - name: nav_fw_pos_z_d
2140 description: "D gain of altitude PID controller (Fixedwing)"
2142 field: bank_fw.pid[PID_POS_Z].D
2145 - name: nav_fw_alt_control_response
2146 description: "Adjusts the deceleration response of fixed wing altitude control as the target altitude is approached. Decrease value to help avoid overshooting the target altitude."
2148 field: fwAltControlResponseFactor
2151 - name: nav_fw_pos_xy_p
2152 description: "P gain of 2D trajectory PID controller. Play with this to get a straight line between waypoints or a straight RTH"
2154 field: bank_fw.pid[PID_POS_XY].P
2157 - name: nav_fw_pos_xy_i
2158 description: "I gain of 2D trajectory PID controller. Too high and there will be overshoot in trajectory. Better start tuning with zero"
2160 field: bank_fw.pid[PID_POS_XY].I
2163 - name: nav_fw_pos_xy_d
2164 description: "D gain of 2D trajectory PID controller. Too high and there will be overshoot in trajectory. Better start tuning with zero"
2166 field: bank_fw.pid[PID_POS_XY].D
2169 - name: nav_fw_heading_p
2170 description: "P gain of Heading Hold controller (Fixedwing)"
2172 field: bank_fw.pid[PID_HEADING].P
2175 - name: nav_fw_pos_hdg_p
2176 description: "P gain of heading PID controller. (Fixedwing, rovers, boats)"
2178 field: bank_fw.pid[PID_POS_HEADING].P
2181 - name: nav_fw_pos_hdg_i
2182 description: "I gain of heading trajectory PID controller. (Fixedwing, rovers, boats)"
2184 field: bank_fw.pid[PID_POS_HEADING].I
2187 - name: nav_fw_pos_hdg_d
2188 description: "D gain of heading trajectory PID controller. (Fixedwing, rovers, boats)"
2190 field: bank_fw.pid[PID_POS_HEADING].D
2193 - name: nav_fw_pos_hdg_pidsum_limit
2194 description: "Output limit for heading trajectory PID controller. (Fixedwing, rovers, boats)"
2196 field: navFwPosHdgPidsumLimit
2197 min: PID_SUM_LIMIT_MIN
2198 max: PID_SUM_LIMIT_MAX
2199 - name: mc_iterm_relax
2200 description: "Iterm relax type. When enabled, Iterm will be relaxed when stick is centered. This will help to reduce bounceback and followthrough on multirotors. It is recommended to enable this feature on all multirotors."
2204 - name: mc_iterm_relax_cutoff
2205 description: "Iterm relax cutoff frequency."
2206 field: iterm_relax_cutoff
2211 description: "D-term multiplier when pilot provides rapid stick input. Lower values give sharper response to stick input, higher values give smoother response."
2213 condition: USE_D_BOOST
2218 description: "D-term multiplier when rapid external conditions are detected. Lower values give sharper response to stick input, higher values give smoother response by scaling D-gains up."
2220 condition: USE_D_BOOST
2224 - name: d_boost_max_at_acceleration
2225 description: "Acceleration threshold for D-term multiplier. When acceleration is above this value, D-term multiplier is set to `d_boost_max`"
2226 field: dBoostMaxAtAlleceleration
2227 condition: USE_D_BOOST
2231 - name: d_boost_gyro_delta_lpf_hz
2232 description: "Cutoff frequency for the low pass filter applied to the gyro delta signal used for D-term boost. Lower value will produce a smoother D-term boost signal, but it will be more delayed."
2233 field: dBoostGyroDeltaLpfHz
2234 condition: USE_D_BOOST
2238 - name: antigravity_gain
2239 description: "Max Antigravity gain. `1` means Antigravity is disabled, `2` means Iterm is allowed to double during rapid throttle movements"
2241 field: antigravityGain
2242 condition: USE_ANTIGRAVITY
2245 - name: antigravity_accelerator
2246 description: "Multiplier for Antigravity gain. The bigger is the difference between actual and filtered throttle input, the bigger Antigravity gain"
2248 field: antigravityAccelerator
2249 condition: USE_ANTIGRAVITY
2252 - name: antigravity_cutoff_lpf_hz
2253 description: "Antigravity cutoff frequenct for Throtte filter. Antigravity is based on the difference between actual and filtered throttle input. The bigger is the difference, the bigger Antigravity gain"
2255 field: antigravityCutoff
2256 condition: USE_ANTIGRAVITY
2260 description: "Allows to set type of PID controller used in control loop. Possible values: `NONE`, `PID`, `PIFF`, `AUTO`. Change only in case of experimental platforms like VTOL, tailsitters, rovers, boats, etc. Airplanes should always use `PIFF` and multirotors `PID`"
2261 field: pidControllerType
2264 - name: mc_cd_lpf_hz
2265 description: "Cutoff frequency for Control Derivative. This controls the cutoff for the LPF that is applied to the CD (Feed Forward) signal to the PID controller. Lower value will produce a smoother CD gain to the controller, but it will be more delayed. Higher values will produce CD gain that may have more noise in the signal depending on your RC link but wil be less delayed."
2267 field: controlDerivativeLpfHz
2270 - name: fw_level_pitch_trim
2271 description: "Pitch trim for self-leveling flight modes. In degrees. +5 means airplane nose should be raised 5 deg from level"
2273 field: fixedWingLevelTrim
2276 - name: smith_predictor_strength
2277 description: "The strength factor of a Smith Predictor of PID measurement. In percents"
2279 field: smithPredictorStrength
2280 condition: USE_SMITH_PREDICTOR
2283 - name: smith_predictor_delay
2284 description: "Expected delay of the gyro signal. In milliseconds"
2286 field: smithPredictorDelay
2287 condition: USE_SMITH_PREDICTOR
2290 - name: smith_predictor_lpf_hz
2291 description: "Cutoff frequency for the Smith Predictor Low Pass Filter"
2293 field: smithPredictorFilterHz
2294 condition: USE_SMITH_PREDICTOR
2297 - name: fw_level_pitch_gain
2298 description: "I-gain for the pitch trim for self-leveling flight modes. Higher values means that AUTOTRIM will be faster but might introduce oscillations"
2300 field: fixedWingLevelTrimGain
2303 - name: fw_iterm_lock_time_max_ms
2304 description: Defines max time in milliseconds for how long ITerm Lock will shut down Iterm after sticks are release
2306 field: fwItermLockTimeMaxMs
2309 - name: fw_iterm_lock_rate_threshold
2310 description: Defines rate percentage when full P I and D attenuation should happen. 100 disables Iterm Lock for P and D term
2311 field: fwItermLockRateLimit
2315 - name: fw_iterm_lock_engage_threshold
2316 description: Defines error rate (in percents of max rate) when Iterm Lock is engaged when sticks are release. Iterm Lock will stay active until error drops below this number
2320 field: fwItermLockEngageThreshold
2322 - name: PG_PID_AUTOTUNE_CONFIG
2323 type: pidAutotuneConfig_t
2324 condition: USE_AUTOTUNE_FIXED_WING
2326 - name: fw_autotune_min_stick
2327 description: "Minimum stick input [%], after applying deadband and expo, to start recording the plane's response to stick input."
2332 - name: fw_autotune_rate_adjustment
2333 description: "`AUTO` and `LIMIT` adjust the rates to match the capabilities of the airplane, with `LIMIT` they are never increased above the starting rates setting. `FIXED` does not adjust the rates. Rates are not changed when tuning in `ANGLE` mode."
2334 default_value: "AUTO"
2335 field: fw_rate_adjustment
2336 table: autotune_rate_adjustment
2338 - name: fw_autotune_max_rate_deflection
2339 description: "The target percentage of maximum mixer output used for determining the rates in `AUTO` and `LIMIT`."
2341 field: fw_max_rate_deflection
2345 - name: PG_POSITION_ESTIMATION_CONFIG
2346 type: positionEstimationConfig_t
2348 - name: inav_auto_mag_decl
2349 description: "Automatic setting of magnetic declination based on GPS position. When used manual magnetic declination is ignored."
2351 field: automatic_mag_declination
2353 - name: inav_gravity_cal_tolerance
2354 description: "Unarmed gravity calibration tolerance level. Won't finish the calibration until estimated gravity error falls below this value."
2356 field: gravity_calibration_tolerance
2359 - name: inav_allow_dead_reckoning
2360 description: "Defines if INAV will dead-reckon over short GPS outages. May also be useful for indoors OPFLOW navigation"
2362 field: allow_dead_reckoning
2364 - name: inav_allow_gps_fix_estimation
2365 description: "Defines if inav will estimate GPS fix with magnetometer and barometer on GPS outages. Enables navigation and RTH without GPS fix on fixed wing. Also see failsafe_gps_fix_estimation_delay."
2366 condition: USE_GPS_FIX_ESTIMATION
2368 field: allow_gps_fix_estimation
2370 - name: inav_reset_altitude
2371 description: "Defines when relative estimated altitude is reset to zero. Variants - `NEVER` (once reference is acquired it's used regardless); `FIRST_ARM` (keep altitude at zero until firstly armed), `EACH_ARM` (altitude is reset to zero on each arming)"
2372 default_value: "FIRST_ARM"
2373 field: reset_altitude_type
2375 - name: inav_reset_home
2376 description: "Allows to chose when the home position is reset. Can help prevent resetting home position after accidental mid-air disarm. Possible values are: NEVER, FIRST_ARM and EACH_ARM"
2377 default_value: "FIRST_ARM"
2378 field: reset_home_type
2380 - name: inav_max_surface_altitude
2381 description: "Max allowed altitude for surface following mode. [cm]"
2383 field: max_surface_altitude
2386 - name: inav_w_z_surface_p
2387 description: "Weight of rangefinder measurements in estimated altitude. Setting is used on both airplanes and multirotors when rangefinder is present and Surface mode enabled"
2388 field: w_z_surface_p
2392 - name: inav_w_z_surface_v
2393 description: "Weight of rangefinder measurements in estimated climb rate. Setting is used on both airplanes and multirotors when rangefinder is present and Surface mode enabled"
2394 field: w_z_surface_v
2398 - name: inav_w_xy_flow_p
2399 description: "Weight of optical flow measurements in estimated UAV position."
2404 - name: inav_w_xy_flow_v
2405 description: "Weight of optical flow measurements in estimated UAV speed."
2410 - name: inav_w_z_baro_p
2411 description: "Weight of barometer measurements in estimated altitude and climb rate. Setting is used on both airplanes and multirotors."
2416 - name: inav_w_z_baro_v
2417 description: "Weight of barometer climb rate measurements in estimated climb rate. Setting is used on both airplanes and multirotors."
2422 - name: inav_w_z_gps_p
2423 description: "Weight of GPS altitude measurements in estimated altitude. Setting is used on both airplanes and multirotors."
2428 - name: inav_w_z_gps_v
2429 description: "Weight of GPS climb rate measurements in estimated climb rate. Setting is used on both airplanes and multirotors."
2434 - name: inav_w_xy_gps_p
2435 description: "Weight of GPS coordinates in estimated UAV position and speed."
2440 - name: inav_w_xy_gps_v
2441 description: "Weight of GPS velocity data in estimated UAV speed"
2446 - name: inav_w_z_res_v
2447 description: "Decay coefficient for estimated climb rate when baro/GPS reference for altitude is lost"
2452 - name: inav_w_xy_res_v
2453 description: "Decay coefficient for estimated velocity when GPS reference for position is lost"
2458 - name: inav_w_acc_bias
2459 description: "Weight for accelerometer drift estimation"
2464 - name: inav_max_eph_epv
2465 description: "Maximum uncertainty value until estimated position is considered valid and is used for navigation [cm]"
2470 - name: inav_baro_epv
2471 description: "Uncertainty value for barometric sensor [cm]"
2476 - name: inav_default_alt_sensor
2477 description: "Sets the default altitude sensor to use. Settings GPS and BARO always use both sensors unless there is an altitude error between the sensors that exceeds a set limit. In this case only the selected sensor will be used while the altitude error limit is exceeded. GPS error limit = 2 * inav_max_eph_epv. BARO error limit = 4 * inav_baro_epv. Settings GPS_ONLY and BARO_ONLY will use only the selected sensor even if the other sensor is working. The other sensor will only be used as a backup if the selected sensor is no longer available to use."
2478 default_value: "GPS"
2479 field: default_alt_sensor
2480 table: default_altitude_source
2482 - name: PG_NAV_CONFIG
2484 headers: ["navigation/navigation.h"]
2486 - name: nav_disarm_on_landing
2487 description: "If set to ON, INAV disarms the FC after landing"
2489 field: general.flags.disarm_on_landing
2491 - name: nav_land_detect_sensitivity
2492 description: "Changes sensitivity of landing detection. Higher values increase speed of detection but also increase risk of false detection. Default value should work in most cases."
2494 field: general.land_detect_sensitivity
2497 - name: nav_landing_bump_detection
2498 description: "Allows immediate landing detection based on G bump at touchdown when set to ON. Requires a barometer and GPS and currently only works for multirotors (Note: will work during Failsafe without need for a GPS)."
2500 field: general.flags.landing_bump_detection
2502 - name: nav_mc_inverted_crash_detection
2503 description: "Setting a value > 0 enables inverted crash detection for multirotors. It will auto disarm in situations where the multirotor has crashed inverted on the ground and can't be manually disarmed due to loss of control or for some other reason. When enabled this setting defines the additional number of seconds before disarm beyond a minimum fixed time delay of 3s. Requires a barometer to work."
2505 field: mc.inverted_crash_detection
2508 - name: nav_mc_althold_throttle
2509 description: "If set to STICK the FC remembers the throttle stick position when enabling ALTHOLD and treats it as the neutral midpoint for holding altitude. If set to MID_STICK or HOVER the neutral midpoint is set to the mid stick position or the hover throttle position respectively."
2510 default_value: "STICK"
2511 field: mc.althold_throttle_type
2512 table: nav_mc_althold_throttle
2513 - name: nav_extra_arming_safety
2514 description: "If set to ON drone won't arm if no GPS fix and any navigation mode like RTH or POSHOLD is configured. ALLOW_BYPASS allows the user to momentarily disable this check by holding yaw high (left stick held at the bottom right in mode 2) when switch arming is used"
2515 default_value: "ALLOW_BYPASS"
2516 field: general.flags.extra_arming_safety
2517 table: nav_extra_arming_safety
2518 - name: nav_user_control_mode
2519 description: "Defines how Pitch/Roll input from RC receiver affects flight in POSHOLD mode: ATTI - pitch/roll controls attitude like in ANGLE mode; CRUISE - pitch/roll controls velocity in forward and right direction."
2520 default_value: "ATTI"
2521 field: general.flags.user_control_mode
2522 table: nav_user_control_mode
2523 - name: nav_position_timeout
2524 description: "If GPS fails wait for this much seconds before switching to emergency landing mode (0 - disable)"
2526 field: general.pos_failure_timeout
2529 - name: nav_wp_load_on_boot
2530 description: "If set to ON, waypoints will be automatically loaded from EEPROM to the FC during startup."
2532 field: general.waypoint_load_on_boot
2534 - name: nav_wp_radius
2535 description: "Waypoint radius [cm]. Waypoint would be considered reached if machine is within this radius"
2537 field: general.waypoint_radius
2540 - name: nav_wp_enforce_altitude
2541 description: "Forces craft to achieve the set WP altitude as well as position before moving to next WP. Position is held and altitude adjusted as required before moving on. 0 = disabled, otherwise setting defines altitude capture tolerance [cm], e.g. 100 means required altitude is achieved when within 100cm of waypoint altitude setting."
2543 field: general.waypoint_enforce_altitude
2546 - name: nav_wp_max_safe_distance
2547 description: "First waypoint in the mission should be closer than this value [m]. A value of 0 disables this check."
2549 field: general.waypoint_safe_distance
2552 - name: nav_wp_mission_restart
2553 description: "Sets restart behaviour for a WP mission when interrupted mid mission. START from first WP, RESUME from last active WP or SWITCH between START and RESUME each time WP Mode is reselected ON. SWITCH effectively allows resuming once only from a previous mid mission waypoint after which the mission will restart from the first waypoint."
2554 default_value: "RESUME"
2555 field: general.flags.waypoint_mission_restart
2556 table: nav_wp_mission_restart
2557 - name: nav_wp_multi_mission_index
2558 description: "Index of active mission selected from multi mission WP entry loaded in flight controller. Limited to a maximum of 9 missions."
2560 field: general.waypoint_multi_mission_index
2561 condition: USE_MULTI_MISSION
2564 - name: nav_fw_wp_tracking_accuracy
2565 description: "Waypoint tracking accuracy forces the craft to quickly head toward and track along the waypoint course line as closely as possible. Setting adjusts tracking deadband distance fom waypoint courseline [m]. Tracking isn't actively controlled within the deadband providing smoother flight adjustments but less accurate tracking. A 2m deadband should work OK in most cases. Setting to 0 disables waypoint tracking accuracy."
2567 field: fw.wp_tracking_accuracy
2570 - name: nav_fw_wp_tracking_max_angle
2571 description: "Sets the maximum allowed alignment convergence angle to the waypoint course line when nav_fw_wp_tracking_accuracy is active [degrees]. Lower values result in smoother alignment with the course line but will take more distance until this is achieved."
2573 field: fw.wp_tracking_max_angle
2576 - name: nav_fw_wp_turn_smoothing
2577 description: "Smooths turns during WP missions by switching to a loiter turn at waypoints. When set to ON the craft will reach the waypoint during the turn. When set to ON-CUT the craft will turn inside the waypoint without actually reaching it (cuts the corner)."
2578 default_value: "OFF"
2579 field: fw.wp_turn_smoothing
2580 table: nav_fw_wp_turn_smoothing
2581 - name: nav_auto_speed
2582 description: "Speed in fully autonomous modes (RTH, WP) [cm/s]. Used for WP mode when no specific WP speed set. [Multirotor only]"
2584 field: general.auto_speed
2587 - name: nav_min_ground_speed
2588 description: "Minimum ground speed for navigation flight modes [m/s]. Currently, this only affects fixed wing. Default 7 m/s."
2590 field: general.min_ground_speed
2593 - name: nav_max_auto_speed
2594 description: "Maximum speed allowed in fully autonomous modes (RTH, WP) [cm/s] [Multirotor only]"
2596 field: general.max_auto_speed
2599 - name: nav_manual_speed
2600 description: "Maximum speed allowed when processing pilot input for POSHOLD/CRUISE control mode [cm/s] [Multirotor only]"
2602 field: general.max_manual_speed
2605 - name: nav_land_minalt_vspd
2606 description: "Vertical descent velocity under nav_land_slowdown_minalt during the RTH landing phase. [cm/s]"
2608 field: general.land_minalt_vspd
2611 - name: nav_land_maxalt_vspd
2612 description: "Vertical descent velocity above nav_land_slowdown_maxalt during the RTH landing phase. [cm/s]"
2614 field: general.land_maxalt_vspd
2617 - name: nav_land_slowdown_minalt
2618 description: "Defines at what altitude the descent velocity should start to be `nav_land_minalt_vspd` [cm]"
2620 field: general.land_slowdown_minalt
2623 - name: nav_land_slowdown_maxalt
2624 description: "Defines at what altitude the descent velocity should start to ramp down from `nav_land_maxalt_vspd` to `nav_land_minalt_vspd` during the RTH landing phase [cm]"
2626 field: general.land_slowdown_maxalt
2629 - name: nav_emerg_landing_speed
2630 description: "Rate of descent UAV will try to maintain when doing emergency descent sequence [cm/s]"
2632 field: general.emerg_descent_rate
2635 - name: nav_min_rth_distance
2636 description: "Minimum distance from homepoint when RTH full procedure will be activated [cm]. Below this distance, the mode will activate at the current location and the final phase is executed (loiter / land). Above this distance, the full procedure is activated, which may include initial climb and flying directly to the homepoint before entering the loiter / land phase."
2638 field: general.min_rth_distance
2641 - name: nav_overrides_motor_stop
2642 description: "When set to OFF the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect on NAV modes which take control of the throttle when combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV"
2643 default_value: "ALL_NAV"
2644 field: general.flags.nav_overrides_motor_stop
2645 table: nav_overrides_motor_stop
2646 - name: nav_fw_soaring_motor_stop
2647 description: "Stops motor when Soaring mode enabled."
2649 field: general.flags.soaring_motor_stop
2651 - name: nav_fw_soaring_pitch_deadband
2652 description: "Pitch Angle deadband when soaring mode enabled (deg). Angle mode inactive within deadband allowing pitch to free float whilst soaring."
2654 field: fw.soaring_pitch_deadband
2657 - name: nav_rth_climb_first
2658 description: "If set to ON or ON_FW_SPIRAL aircraft will climb to nav_rth_altitude first before turning to head home. If set to OFF aircraft will turn and head home immediately climbing on the way. For a fixed wing ON will use a linear climb, ON_FW_SPIRAL will use a loiter turning climb with climb rate set by nav_auto_climb_rate, turn rate set by nav_fw_loiter_radius (ON_FW_SPIRAL is a fixed wing setting and behaves the same as ON for a multirotor)"
2660 field: general.flags.rth_climb_first
2661 table: nav_rth_climb_first
2662 - name: nav_rth_climb_first_stage_mode
2663 description: "This determines how rth_climb_first_stage_altitude is used. Default is AT_LEAST."
2664 default_value: "AT_LEAST"
2665 field: general.flags.rth_climb_first_stage_mode
2666 table: nav_rth_climb_first_stage_modes
2667 - name: nav_rth_climb_first_stage_altitude
2668 description: "The altitude [cm] at which climb first will transition to turn first. How the altitude is used, is determined by nav_rth_climb_first_stage_mode. Default=0; feature disabled."
2670 field: general.rth_climb_first_stage_altitude
2672 - name: nav_rth_climb_ignore_emerg
2673 description: "If set to ON, aircraft will execute initial climb regardless of position sensor (GPS) status."
2675 field: general.flags.rth_climb_ignore_emerg
2677 - name: nav_rth_tail_first
2678 description: "If set to ON drone will return tail-first. Obviously meaningless for airplanes."
2680 field: general.flags.rth_tail_first
2682 - name: nav_rth_allow_landing
2683 description: "If set to ON drone will land as a last phase of RTH."
2684 default_value: "ALWAYS"
2685 field: general.flags.rth_allow_landing
2686 table: nav_rth_allow_landing
2687 - name: nav_rth_fs_landing_delay
2688 description: "If landing is active on Failsafe and this is above 0. The aircraft will hover or loiter for X seconds before performing the landing. If the battery enters the warning or critical levels, the land will proceed. Default = 0 [seconds]"
2692 field: general.rth_fs_landing_delay
2693 - name: nav_rth_alt_mode
2694 description: "Configure how the aircraft will manage altitude on the way home, see Navigation modes on wiki for more details"
2695 default_value: "AT_LEAST"
2696 field: general.flags.rth_alt_control_mode
2697 table: nav_rth_alt_mode
2698 - name: nav_rth_alt_control_override
2699 description: "If set to ON RTH altitude and CLIMB FIRST settings can be overridden during the RTH climb phase using full pitch or roll stick held for > 1 second. RTH altitude is reset to the current altitude using pitch down stick. RTH CLIMB FIRST is overridden using right roll stick so craft turns and heads directly to home (CLIMB FIRST override only works for fixed wing)"
2701 field: general.flags.rth_alt_control_override
2703 - name: nav_rth_abort_threshold
2704 description: "RTH sanity checking feature will notice if distance to home is increasing during RTH and once amount of increase exceeds the threshold defined by this parameter, instead of continuing RTH machine will enter emergency landing, self-level and go down safely. Default is 500m which is safe enough for both multirotor machines and airplanes. Set to 0 to disable. [cm]"
2705 default_value: 50000
2706 field: general.rth_abort_threshold
2709 - name: nav_max_terrain_follow_alt
2710 field: general.max_terrain_follow_altitude
2711 default_value: "100"
2712 description: "Max allowed above the ground altitude for terrain following mode [cm]"
2715 - name: nav_max_altitude
2716 field: general.max_altitude
2717 description: "Max allowed altitude (above Home Point) that applies to all NAV modes (including Altitude Hold). 0 means limit is disabled"
2721 - name: nav_rth_altitude
2722 description: "Used in EXTRA, FIXED and AT_LEAST rth alt modes [cm] (Default 1000 means 10 meters)"
2724 field: general.rth_altitude
2726 - name: nav_rth_home_altitude
2727 description: "Aircraft will climb/descend to this altitude after reaching home if landing is not enabled. Set to 0 to stay at `nav_rth_altitude` (default) [cm]"
2729 field: general.rth_home_altitude
2731 - name: nav_rth_linear_descent_start_distance
2732 description: The distance [m] away from home to start the linear descent. 0 = immediately (original linear descent behaviour)
2736 field: general.rth_linear_descent_start_distance
2737 - name: nav_rth_use_linear_descent
2738 description: If enabled, the aircraft will gradually descent to the nav_rth_home_altitude en route. The distance from home to start the descent can be set with `nav_rth_linear_descent_start_distance`.
2741 field: general.flags.rth_use_linear_descent
2742 - name: nav_rth_trackback_mode
2743 description: "Useage modes for RTH Trackback. OFF = disabled, ON = Normal and Failsafe RTH, FS = Failsafe RTH only."
2744 default_value: "OFF"
2745 field: general.flags.rth_trackback_mode
2746 table: rth_trackback_mode
2747 - name: nav_rth_trackback_distance
2748 description: "Maximum distance allowed for RTH trackback. Normal RTH is executed once this distance is exceeded [m]."
2750 field: general.rth_trackback_distance
2753 - name: safehome_max_distance
2754 description: "In order for a safehome to be used, it must be less than this distance (in cm) from the arming point."
2755 default_value: 20000
2756 field: general.safehome_max_distance
2759 - name: safehome_usage_mode
2760 description: "Used to control when safehomes will be used. Possible values are `OFF`, `RTH` and `RTH_FS`. See [Safehome documentation](Safehomes.md#Safehome) for more information."
2761 default_value: "RTH"
2762 field: general.flags.safehome_usage_mode
2763 table: safehome_usage_mode
2764 - name: nav_mission_planner_reset
2765 description: "With Reset ON WP Mission Planner waypoint count can be reset to 0 by toggling the mode switch ON-OFF-ON."
2767 field: general.flags.mission_planner_reset
2769 - name: nav_cruise_yaw_rate
2770 description: "Max YAW rate when NAV COURSE HOLD/CRUISE mode is enabled. Set to 0 to disable on fixed wing (Note: On multirotor setting to 0 will disable Course Hold/Cruise mode completely) [dps]"
2772 field: general.cruise_yaw_rate
2775 - name: nav_mc_bank_angle
2776 description: "Maximum banking angle (deg) that multicopter navigation is allowed to set. Machine must be able to satisfy this angle without loosing altitude"
2778 field: mc.max_bank_angle
2781 - name: nav_mc_auto_climb_rate
2782 description: "Maximum climb/descent rate that UAV is allowed to reach during navigation modes. [cm/s]"
2784 field: mc.max_auto_climb_rate
2787 - name: nav_mc_manual_climb_rate
2788 description: "Maximum climb/descent rate firmware is allowed when processing pilot input for ALTHOLD control mode [cm/s]"
2790 field: mc.max_manual_climb_rate
2793 - name: nav_auto_disarm_delay
2794 description: "Delay before craft disarms when `nav_disarm_on_landing` is set (ms)"
2796 field: general.auto_disarm_delay
2799 - name: nav_mc_braking_speed_threshold
2800 description: "min speed in cm/s above which braking can happen"
2802 field: mc.braking_speed_threshold
2803 condition: USE_MR_BRAKING_MODE
2806 - name: nav_mc_braking_disengage_speed
2807 description: "braking is disabled when speed goes below this value"
2809 field: mc.braking_disengage_speed
2810 condition: USE_MR_BRAKING_MODE
2813 - name: nav_mc_braking_timeout
2814 description: "timeout in ms for braking"
2816 field: mc.braking_timeout
2817 condition: USE_MR_BRAKING_MODE
2820 - name: nav_mc_braking_boost_factor
2821 description: "acceleration factor for BOOST phase"
2823 field: mc.braking_boost_factor
2824 condition: USE_MR_BRAKING_MODE
2827 - name: nav_mc_braking_boost_timeout
2828 description: "how long in ms BOOST phase can happen"
2830 field: mc.braking_boost_timeout
2831 condition: USE_MR_BRAKING_MODE
2834 - name: nav_mc_braking_boost_speed_threshold
2835 description: "BOOST can be enabled when speed is above this value"
2837 field: mc.braking_boost_speed_threshold
2838 condition: USE_MR_BRAKING_MODE
2841 - name: nav_mc_braking_boost_disengage_speed
2842 description: "BOOST will be disabled when speed goes below this value"
2844 field: mc.braking_boost_disengage_speed
2845 condition: USE_MR_BRAKING_MODE
2848 - name: nav_mc_braking_bank_angle
2849 description: "max angle that MR is allowed to bank in BOOST mode"
2851 field: mc.braking_bank_angle
2852 condition: USE_MR_BRAKING_MODE
2855 - name: nav_mc_pos_deceleration_time
2856 description: "Used for stoping distance calculation. Stop position is computed as _speed_ * _nav_mc_pos_deceleration_time_ from the place where sticks are released. Braking mode overrides this setting"
2858 field: mc.posDecelerationTime
2861 - name: nav_mc_pos_expo
2862 description: "Expo for PosHold control"
2864 field: mc.posResponseExpo
2867 - name: nav_mc_wp_slowdown
2868 description: "When ON, NAV engine will slow down when switching to the next waypoint. This prioritizes turning over forward movement. When OFF, NAV engine will continue to the next waypoint and turn as it goes."
2870 field: mc.slowDownForTurning
2872 - name: nav_fw_bank_angle
2873 description: "Max roll angle when rolling / turning in GPS assisted modes, is also restrained by global max_angle_inclination_rll"
2875 field: fw.max_bank_angle
2878 - name: nav_fw_auto_climb_rate
2879 description: "Maximum climb/descent rate that UAV is allowed to reach during navigation modes. [cm/s]"
2881 field: fw.max_auto_climb_rate
2884 - name: nav_fw_manual_climb_rate
2885 description: "Maximum climb/descent rate firmware is allowed when processing pilot input for ALTHOLD control mode [cm/s]"
2887 field: fw.max_manual_climb_rate
2890 - name: nav_fw_climb_angle
2891 description: "Max pitch angle when climbing in GPS assisted modes, is also restrained by global max_angle_inclination_pit"
2893 field: fw.max_climb_angle
2896 - name: nav_fw_dive_angle
2897 description: "Max negative pitch angle when diving in GPS assisted modes, is also restrained by global max_angle_inclination_pit"
2899 field: fw.max_dive_angle
2902 - name: nav_fw_pitch2thr_smoothing
2903 description: "How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by pitch_to_throttle_thresh."
2905 field: fw.pitch_to_throttle_smooth
2908 - name: fw_min_throttle_down_pitch
2909 description: "Automatic pitch down angle when throttle is at 0 in angle mode. Progressively applied between cruise throttle and zero throttle (decidegrees)"
2911 field: fw.minThrottleDownPitchAngle
2914 - name: nav_fw_pitch2thr_threshold
2915 description: "Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees]"
2917 field: fw.pitch_to_throttle_thresh
2920 - name: nav_fw_loiter_radius
2921 description: "PosHold radius. 3000 to 7500 is a good value (30-75m) [cm]"
2923 field: fw.loiter_radius
2926 - name: fw_loiter_direction
2927 description: "Direction of loitering: center point on right wing (clockwise - default), or center point on left wing (counterclockwise). If equal YAW then can be changed in flight using a yaw stick."
2928 default_value: "RIGHT"
2929 field: fw.loiter_direction
2931 - name: nav_fw_cruise_speed
2932 description: "Speed for the plane/wing at cruise throttle used for remaining flight time/distance estimation in cm/s"
2934 field: fw.cruise_speed
2937 - name: nav_fw_control_smoothness
2938 description: "How smoothly the autopilot controls the airplane to correct the navigation error"
2940 field: fw.control_smoothness
2943 - name: nav_fw_land_dive_angle
2944 description: "Dive angle that airplane will use during final landing phase. During dive phase, motor is stopped or IDLE and roll control is locked to 0 degrees"
2946 field: fw.land_dive_angle
2949 - name: nav_fw_launch_velocity
2950 description: "Forward velocity threshold for swing-launch detection [cm/s]"
2952 field: fw.launch_velocity_thresh
2955 - name: nav_fw_launch_accel
2956 description: "Forward acceleration threshold for bungee launch or throw launch [cm/s/s], 1G = 981 cm/s/s"
2958 field: fw.launch_accel_thresh
2961 - name: nav_fw_launch_max_angle
2962 description: "Max tilt angle (pitch/roll combined) to consider launch successful. Set to 180 to disable completely [deg]"
2964 field: fw.launch_max_angle
2967 - name: nav_fw_launch_detect_time
2968 description: "Time for which thresholds have to breached to consider launch happened [ms]"
2970 field: fw.launch_time_thresh
2973 - name: nav_fw_launch_idle_motor_delay
2974 description: "Delay between raising throttle and motor starting at idle throttle (ms)"
2976 field: fw.launch_idle_motor_timer
2979 - name: nav_fw_launch_wiggle_to_wake_idle
2980 description: "Trigger the idle throttle by wiggling the plane. 0 = disabled. 1 and 2 signify 1 or 2 yaw wiggles to activate. 1 wiggle has a higher detection point, for airplanes without a tail. 2 wiggles has a lower detection point, but requires the repeated action. This is intended for larger models and airplanes with tails."
2981 field: fw.launch_wiggle_wake_idle
2986 - name: nav_fw_launch_motor_delay
2987 description: "Delay between detected launch and launch sequence start and throttling up (ms)"
2989 field: fw.launch_motor_timer
2992 - name: nav_fw_launch_spinup_time
2993 description: "Time to bring power from minimum throttle to nav_fw_launch_thr - to avoid big stress on ESC and large torque from propeller"
2995 field: fw.launch_motor_spinup_time
2998 - name: nav_fw_launch_end_time
2999 description: "Time for the transition of throttle and pitch angle, between the launch state and the subsequent flight mode [ms]"
3001 field: fw.launch_end_time
3004 - name: nav_fw_launch_min_time
3005 description: "Allow launch mode to execute at least this time (ms) and ignore stick movements [0-60000]."
3007 field: fw.launch_min_time
3010 - name: nav_fw_launch_timeout
3011 description: "Maximum time for launch sequence to be executed. After this time LAUNCH mode will be turned off and regular flight mode will take over (ms)"
3013 field: fw.launch_timeout
3015 - name: nav_fw_launch_max_altitude
3016 description: "Altitude (centimeters) at which LAUNCH mode will be turned off and regular flight mode will take over [0-60000]."
3018 field: fw.launch_max_altitude
3021 - name: nav_fw_launch_climb_angle
3022 description: "Climb angle (attitude of model, not climb slope) for launch sequence (degrees), is also restrained by global max_angle_inclination_pit"
3024 field: fw.launch_climb_angle
3027 - name: nav_fw_launch_manual_throttle
3028 description: "Allows launch with manually controlled throttle. INAV only levels wings and controls climb pitch during launch. Throttle is controlled directly by throttle stick movement. IF USED WITHOUT A GPS LOCK plane must be launched immediately after throttle is increased to avoid issues with climb out stabilisation and the launch ending sooner than expected (launch end timer starts as soon as the throttle stick is raised)."
3030 field: fw.launch_manual_throttle
3032 - name: nav_fw_launch_land_abort_deadband
3033 description: "Launch and landing abort stick deadband in [r/c points], applied after r/c deadband and expo. The Roll/Pitch stick needs to be deflected beyond this deadband to abort the launch or landing."
3035 field: fw.launch_land_abort_deadband
3038 - name: nav_fw_allow_manual_thr_increase
3039 description: "Enable the possibility to manually increase the throttle in auto throttle controlled modes for fixed wing"
3041 field: fw.allow_manual_thr_increase
3043 - name: nav_use_fw_yaw_control
3044 description: "Enables or Disables the use of the heading PID controller on fixed wing. Heading PID controller is always enabled for rovers and boats"
3046 field: fw.useFwNavYawControl
3048 - name: nav_fw_yaw_deadband
3049 description: "Deadband for heading trajectory PID controller. When heading error is below the deadband, controller assumes that vehicle is on course"
3051 field: fw.yawControlDeadband
3055 - name: PG_TELEMETRY_CONFIG
3056 type: telemetryConfig_t
3057 headers: ["io/serial.h", "telemetry/telemetry.h", "telemetry/sim.h"]
3058 condition: USE_TELEMETRY
3060 - name: telemetry_switch
3061 description: "Which aux channel to use to change serial output & baud rate (MSP / Telemetry). It disables automatic switching to Telemetry when armed."
3064 - name: telemetry_inverted
3065 description: "Determines if the telemetry protocol default signal inversion is reversed. This should be OFF in most cases unless a custom or hacked RX is used."
3068 - name: frsky_pitch_roll
3069 description: "S.Port telemetry: Send pitch and roll degrees*10 instead of raw accelerometer data"
3072 - name: frsky_use_legacy_gps_mode_sensor_ids
3073 description: "S.Port telemetry: If `ON`, send the legacy telemetry IDs for modes (Tmp1) and GNSS (Tmp2). These are old IDs, deprecated, and will be removed in INAV 10.0. Tools and scripts using these IDs should be updated to use the new IDs of **470** for Modes and **480** for GNSS. Default: 'OFF'"
3076 - name: report_cell_voltage
3077 description: "S.Port and IBUS telemetry: Send the average cell voltage if set to ON"
3080 - name: hott_alarm_sound_interval
3081 description: "Battery alarm delay in seconds for Hott telemetry"
3083 field: hottAlarmSoundInterval
3086 - name: telemetry_halfduplex
3087 description: "S.Port telemetry only: Turn UART into UNIDIR for usage on F1 and F4 target. See Telemetry.md for details"
3091 - name: smartport_fuel_unit
3092 description: "S.Port telemetry only: Unit of the value sent with the `FUEL` ID (FrSky D-Series always sends percent). [PERCENT/MAH/MWH]"
3093 default_value: "MAH"
3094 field: smartportFuelUnit
3095 condition: USE_TELEMETRY_SMARTPORT
3097 table: smartport_fuel_unit
3098 - name: ibus_telemetry_type
3099 description: "Type compatibility ibus telemetry for transmitters. See Telemetry.md label IBUS for details."
3101 field: ibusTelemetryType
3104 - name: ltm_update_rate
3105 description: "Defines the LTM update rate (use of bandwidth [NORMAL/MEDIUM/SLOW]). See Telemetry.md, LTM section for details."
3106 default_value: "NORMAL"
3107 field: ltmUpdateRate
3108 condition: USE_TELEMETRY_LTM
3110 - name: sim_ground_station_number
3111 description: "Number of phone that is used to communicate with SIM module. Messages / calls from other numbers are ignored. If undefined, can be set by calling or sending a message to the module."
3113 field: simGroundStationNumber
3114 condition: USE_TELEMETRY_SIM
3116 description: "PIN code for the SIM module"
3117 default_value: "0000"
3119 condition: USE_TELEMETRY_SIM
3120 - name: sim_transmit_interval
3121 description: "Text message transmission interval in seconds for SIM module. Minimum value: 10"
3123 field: simTransmitInterval
3124 condition: USE_TELEMETRY_SIM
3126 min: SIM_MIN_TRANSMIT_INTERVAL
3128 - name: sim_transmit_flags
3129 description: "Bitmask specifying text message transmit condition flags for the SIM module. 1: continuous transmission, 2: continuous transmission in failsafe mode, 4: continuous transmission when GPS signal quality is low, 8: acceleration events, 16: continuous transmission when altitude is below `sim_low_altitude`"
3130 default_value: :SIM_TX_FLAG_FAILSAFE
3131 field: simTransmitFlags
3132 condition: USE_TELEMETRY_SIM
3134 - name: acc_event_threshold_high
3135 description: "Acceleration threshold [cm/s/s] for impact / high g event text messages sent by SIM module. Acceleration values greater than 4 g can occur in fixed wing flight without an impact, so a setting of 4000 or greater is suggested. 0 = detection off."
3137 field: accEventThresholdHigh
3138 condition: USE_TELEMETRY_SIM
3142 - name: acc_event_threshold_low
3143 description: "Acceleration threshold [cm/s/s] for low-g / freefall detection text messages sent by SIM module. A setting of less than 100 is suggested. Valid values: [0-900], 0 = detection off."
3145 field: accEventThresholdLow
3146 condition: USE_TELEMETRY_SIM
3150 - name: acc_event_threshold_neg_x
3151 description: "Acceleration threshold [cm/s/s] for backwards acceleration / fixed wing landing detection text messages sent by SIM module. Suggested value for fixed wing: 1100. 0 = detection off."
3153 field: accEventThresholdNegX
3154 condition: USE_TELEMETRY_SIM
3158 - name: sim_low_altitude
3159 description: "Threshold for low altitude warning messages sent by SIM module when the 'L' transmit flag is set in `sim_transmit_flags`."
3160 default_value: -32767
3161 field: simLowAltitude
3162 condition: USE_TELEMETRY_SIM
3166 - name: mavlink_ext_status_rate
3167 field: mavlink.extended_status_rate
3168 description: "Rate of the extended status message for MAVLink telemetry"
3173 - name: mavlink_rc_chan_rate
3174 description: "Rate of the RC channels message for MAVLink telemetry"
3175 field: mavlink.rc_channels_rate
3180 - name: mavlink_pos_rate
3181 description: "Rate of the position message for MAVLink telemetry"
3182 field: mavlink.position_rate
3187 - name: mavlink_extra1_rate
3188 description: "Rate of the extra1 message for MAVLink telemetry"
3189 field: mavlink.extra1_rate
3194 - name: mavlink_extra2_rate
3195 description: "Rate of the extra2 message for MAVLink telemetry"
3196 field: mavlink.extra2_rate
3201 - name: mavlink_extra3_rate
3202 description: "Rate of the extra3 message for MAVLink telemetry"
3203 field: mavlink.extra3_rate
3208 - name: mavlink_version
3209 field: mavlink.version
3210 description: "Version of MAVLink to use"
3215 - name: mavlink_min_txbuffer
3216 field: mavlink.min_txbuff
3217 description: "Minimum percent of TX buffer space free, before attempting to transmit telemetry. Requuires RADIO_STATUS messages to be processed. 0 = always transmits."
3221 - name: mavlink_radio_type
3222 description: "Mavlink radio type. Affects how RSSI and LQ are reported on OSD."
3223 field: mavlink.radio_type
3224 table: mavlink_radio_type
3225 default_value: "GENERIC"
3228 - name: PG_OSD_CONFIG
3230 headers: ["io/osd.h", "drivers/osd.h"]
3233 - name: osd_telemetry
3234 description: "To enable OSD telemetry for antenna tracker. Possible values are `OFF`, `ON` and `TEST`"
3235 table: osd_telemetry
3238 default_value: "OFF"
3239 - name: osd_video_system
3240 description: "Video system used. Possible values are `AUTO`, `PAL`, `NTSC`, `HDZERO`, 'DJIWTF', 'AVATAR' and `BF43COMPAT`"
3241 default_value: "AUTO"
3242 table: osd_video_system
3245 - name: osd_row_shiftdown
3246 description: "Number of rows to shift the OSD display (increase if top rows are cut off)"
3248 field: row_shiftdown
3251 - name: osd_msp_displayport_fullframe_interval
3252 description: "Full Frame redraw interval for MSP DisplayPort [deciseconds]. This is how often a full frame update is sent to the DisplayPort, to cut down on OSD artifacting. The default value should be fine for most pilots. Though long range pilots may benefit from increasing the refresh time, especially near the edge of range. -1 = disabled (legacy mode) | 0 = every frame (not recommended) | default = 10 (1 second)"
3257 field: msp_displayport_fullframe_interval
3259 description: "IMPERIAL, METRIC, UK"
3260 default_value: "METRIC"
3264 - name: osd_stats_energy_unit
3265 description: "Unit used for the drawn energy in the OSD stats [MAH/WH] (milliAmpere hour/ Watt hour)"
3266 default_value: "MAH"
3267 field: stats_energy_unit
3268 table: osd_stats_energy_unit
3270 - name: osd_stats_page_auto_swap_time
3271 description: "Auto swap display time interval between disarm stats pages (seconds). Reverts to manual control when Roll stick used to change pages. Disabled when set to 0."
3273 field: stats_page_auto_swap_time
3276 - name: osd_stats_show_metric_efficiency
3277 description: "Enabling this option will show metric efficiency statistics on the post flight stats screen. In addition to the efficiency statistics in your chosen units."
3280 field: stats_show_metric_efficiency
3281 - name: osd_rssi_alarm
3282 description: "Value below which to make the OSD RSSI indicator blink"
3287 - name: osd_time_alarm
3288 description: "Value above which to make the OSD flight time indicator blink (minutes)"
3293 - name: osd_alt_alarm
3294 description: "Value above which to make the OSD relative altitude indicator blink (meters)"
3299 - name: osd_dist_alarm
3300 description: "Value above which to make the OSD distance from home indicator blink (meters)"
3305 - name: osd_neg_alt_alarm
3306 description: "Value below which (negative altitude) to make the OSD relative altitude indicator blink (meters)"
3308 field: neg_alt_alarm
3311 - name: osd_current_alarm
3312 description: "Value above which the OSD current consumption element will start blinking. Measured in full Amperes."
3314 field: current_alarm
3317 - name: osd_gforce_alarm
3318 description: "Value above which the OSD g force indicator will blink (g)"
3323 - name: osd_gforce_axis_alarm_min
3324 description: "Value under which the OSD axis g force indicators will blink (g)"
3326 field: gforce_axis_alarm_min
3329 - name: osd_gforce_axis_alarm_max
3330 description: "Value above which the OSD axis g force indicators will blink (g)"
3332 field: gforce_axis_alarm_max
3335 - name: osd_imu_temp_alarm_min
3336 description: "Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3338 field: imu_temp_alarm_min
3341 - name: osd_imu_temp_alarm_max
3342 description: "Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3344 field: imu_temp_alarm_max
3347 - name: osd_esc_temp_alarm_max
3348 description: "Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3350 field: esc_temp_alarm_max
3353 - name: osd_esc_temp_alarm_min
3354 description: "Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3356 field: esc_temp_alarm_min
3359 - name: osd_baro_temp_alarm_min
3360 description: "Temperature under which the baro temperature OSD element will start blinking (decidegrees centigrade)"
3362 field: baro_temp_alarm_min
3366 - name: osd_baro_temp_alarm_max
3367 description: "Temperature above which the baro temperature OSD element will start blinking (decidegrees centigrade)"
3369 field: baro_temp_alarm_max
3373 - name: osd_snr_alarm
3374 condition: USE_SERIALRX_CRSF || USE_RX_MSP
3375 description: "Value below which Crossfire SNR Alarm pops-up. (dB)"
3380 - name: osd_link_quality_alarm
3381 condition: USE_SERIALRX_CRSF || USE_RX_MSP
3382 description: "LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%"
3384 field: link_quality_alarm
3387 - name: osd_rssi_dbm_alarm
3388 condition: USE_SERIALRX_CRSF || USE_RX_MSP
3389 description: "RSSI dBm indicator blinks below this value [dBm]. 0 disables this alarm"
3391 field: rssi_dbm_alarm
3394 - name: osd_rssi_dbm_max
3395 condition: USE_SERIALRX_CRSF || USE_RX_MSP
3396 description: "RSSI dBm upper end of curve. Perfect rssi (max) = 100%"
3401 - name: osd_rssi_dbm_min
3402 condition: USE_SERIALRX_CRSF || USE_RX_MSP
3403 description: "RSSI dBm lower end of curve or RX sensitivity level. Worst rssi (min) = 0%"
3408 - name: osd_temp_label_align
3409 description: "Allows to chose between left and right alignment for the OSD temperature sensor labels. Valid values are `LEFT` and `RIGHT`"
3410 default_value: "LEFT"
3411 field: temp_label_align
3412 condition: USE_TEMPERATURE_SENSOR
3413 table: osd_alignment
3415 - name: osd_airspeed_alarm_min
3416 condition: USE_PITOT
3417 description: "Airspeed under which the airspeed OSD element will start blinking (cm/s)"
3419 field: airspeed_alarm_min
3421 max: 27000 # (1000km/h * 1000 * 100 / 60 / 60)
3422 - name: osd_airspeed_alarm_max
3423 condition: USE_PITOT
3424 description: "Airspeed above which the airspeed OSD element will start blinking (cm/s)"
3426 field: airspeed_alarm_max
3428 max: 27000 # (1000km/h * 1000 * 100 / 60 / 60)
3429 - name: osd_ahi_reverse_roll
3430 description: "Switches the artificial horizon in the OSD to instead be a bank indicator, by reversing the direction of its movement."
3431 field: ahi_reverse_roll
3434 - name: osd_ahi_max_pitch
3435 description: "Max pitch, in degrees, for OSD artificial horizon"
3437 field: ahi_max_pitch
3441 - name: osd_crosshairs_style
3442 description: "To set the visual type for the crosshair"
3443 default_value: "DEFAULT"
3444 field: crosshairs_style
3445 table: osd_crosshairs_style
3447 - name: osd_crsf_lq_format
3448 description: "To select LQ format"
3449 default_value: "TYPE1"
3450 field: crsf_lq_format
3451 table: osd_crsf_lq_format
3453 - name: osd_horizon_offset
3454 description: "To vertically adjust the whole OSD and AHI and scrolling bars"
3456 field: horizon_offset
3459 - name: osd_camera_uptilt
3460 description: "Set the camera uptilt for the FPV camera in degres, positive is up, negative is down, relative to the horizontal. Used for correct display of HUD items and AHI (when enabled)."
3462 field: camera_uptilt
3465 - name: osd_ahi_camera_uptilt_comp
3466 description: "When set to `ON`, the AHI position is adjusted by `osd_camera_uptilt`. For example, with a cammera uptilt of 30 degrees, the AHI will appear in the middle of the OSD when the aircraft is pitched forward 30 degrees. When set to `OFF`, the AHI will appear in the center of the OSD regardless of camera angle, but can still be shifted up and down using `osd_horizon_offset` (`osd_ahi_vertical_offset` for pixel-OSD)."
3468 field: ahi_camera_uptilt_comp
3470 - name: osd_camera_fov_h
3471 description: "Horizontal field of view for the camera in degres"
3476 - name: osd_camera_fov_v
3477 description: "Vertical field of view for the camera in degres"
3482 - name: osd_hud_margin_h
3483 description: "Left and right margins for the hud area"
3488 - name: osd_hud_margin_v
3489 description: "Top and bottom margins for the hud area"
3494 - name: osd_hud_homing
3495 description: "To display little arrows around the crossair showing where the home point is in the hud"
3499 - name: osd_hud_homepoint
3500 description: "To 3D-display the home point location in the hud"
3502 field: hud_homepoint
3504 - name: osd_hud_radar_disp
3505 description: "Maximum count of nearby aircrafts or points of interest to display in the hud, as sent from an ESP32 LoRa module. Set to 0 to disable (show nothing). The nearby aircrafts will appear as markers A, B, C, etc"
3507 field: hud_radar_disp
3510 - name: osd_hud_radar_range_min
3511 description: "In meters, radar aircrafts closer than this will not be displayed in the hud"
3513 field: hud_radar_range_min
3516 - name: osd_hud_radar_range_max
3517 description: "In meters, radar aircrafts further away than this will not be displayed in the hud"
3519 field: hud_radar_range_max
3522 - name: osd_hud_radar_alt_difference_display_time
3523 description: "Time in seconds to display the altitude difference in radar"
3524 field: hud_radar_alt_difference_display_time
3528 - name: osd_hud_radar_distance_display_time
3529 description: "Time in seconds to display the distance in radar"
3530 field: hud_radar_distance_display_time
3534 - name: osd_radar_peers_display_time
3535 description: "Time in seconds to display next peer "
3536 field: radar_peers_display_time
3540 - name: osd_hud_wp_disp
3541 description: "How many navigation waypoints are displayed, set to 0 (zero) to disable. As sample, if set to 2, and you just passed the 3rd waypoint of the mission, you'll see markers for the 4th waypoint (marked 1) and the 5th waypoint (marked 2)"
3546 - name: osd_left_sidebar_scroll
3547 description: "Scroll type for the left sidebar"
3548 field: left_sidebar_scroll
3549 table: osd_sidebar_scroll
3552 - name: osd_right_sidebar_scroll
3553 description: "Scroll type for the right sidebar"
3554 field: right_sidebar_scroll
3555 table: osd_sidebar_scroll
3558 - name: osd_sidebar_scroll_arrows
3559 description: "Show arrows for scrolling the sidebars"
3560 field: sidebar_scroll_arrows
3563 - name: osd_main_voltage_decimals
3564 description: "Number of decimals for the battery voltages displayed in the OSD [1-2]."
3566 field: main_voltage_decimals
3569 - name: osd_decimals_altitude
3570 description: "Number of decimals for the altitude displayed in the OSD [3-5]."
3572 field: decimals_altitude
3576 - name: osd_decimals_distance
3577 description: "Number of decimals for distance displayed in the OSD [3-5]. This includes distance from home, total distance, and distance remaining."
3579 field: decimals_distance
3583 - name: osd_coordinate_digits
3584 description: "Number of digits for the coordinates displayed in the OSD [8-11]."
3585 field: coordinate_digits
3589 - name: osd_adsb_distance_warning
3590 description: "Distance in meters of ADSB aircraft that is displayed"
3591 default_value: 20000
3593 field: adsb_distance_warning
3597 - name: osd_adsb_distance_alert
3598 description: "Distance inside which ADSB data flashes for proximity warning"
3601 field: adsb_distance_alert
3605 - name: osd_adsb_ignore_plane_above_me_limit
3606 description: "Ignore adsb planes above, limit, 0 disabled (meters)"
3609 field: adsb_ignore_plane_above_me_limit
3613 - name: osd_estimations_wind_compensation
3614 description: "Use wind estimation for remaining flight time/distance estimation"
3616 condition: USE_WIND_ESTIMATOR
3617 field: estimations_wind_compensation
3619 - name: osd_estimations_wind_mps
3620 description: "Wind speed estimation in m/s"
3622 condition: USE_WIND_ESTIMATOR
3623 field: estimations_wind_mps
3625 - name: osd_failsafe_switch_layout
3626 description: "If enabled the OSD automatically switches to the first layout during failsafe"
3629 - name: osd_plus_code_digits
3630 description: "Numer of plus code digits before shortening with `osd_plus_code_short`. Precision at the equator: 10=13.9x13.9m; 11=2.8x3.5m; 12=56x87cm; 13=11x22cm."
3631 field: plus_code_digits
3635 - name: osd_plus_code_short
3636 description: "Number of leading digits removed from plus code. Removing 2, 4 and 6 digits requires a reference location within, respectively, ~800km, ~40 km and ~2km to recover the original coordinates."
3637 field: plus_code_short
3639 table: osd_plus_code_short
3640 - name: osd_ahi_style
3641 description: "Sets OSD Artificial Horizon style \"DEFAULT\" or \"LINE\" for the FrSky Graphical OSD."
3643 default_value: "DEFAULT"
3644 table: osd_ahi_style
3646 - name: osd_force_grid
3650 description: Force OSD to work in grid mode even if the OSD device supports pixel level access (mainly used for development)
3651 - name: osd_ahi_bordered
3654 description: Shows a border/corners around the AHI region (pixel OSD only)
3656 - name: osd_ahi_width
3659 description: AHI width in pixels (pixel OSD only)
3661 - name: osd_ahi_height
3664 description: AHI height in pixels (pixel OSD only)
3666 - name: osd_ahi_vertical_offset
3667 field: ahi_vertical_offset
3670 description: AHI vertical offset from center (pixel OSD only)
3672 - name: osd_sidebar_horizontal_offset
3673 field: sidebar_horizontal_offset
3677 description: Sidebar horizontal offset from default position. Positive values move the sidebars closer to the edges.
3678 - name: osd_left_sidebar_scroll_step
3679 field: left_sidebar_scroll_step
3682 description: How many units each sidebar step represents. 0 means the default value for the scroll type.
3683 - name: osd_right_sidebar_scroll_step
3684 field: right_sidebar_scroll_step
3687 description: Same as left_sidebar_scroll_step, but for the right sidebar
3688 - name: osd_sidebar_height
3689 field: sidebar_height
3693 description: Height of sidebars in rows. 0 leaves only the level indicator arrows (Not for pixel OSD)
3694 - name: osd_ahi_pitch_interval
3695 field: ahi_pitch_interval
3699 description: Draws AHI at increments of the set pitch interval over the full pitch range. AHI line is drawn with ends offset when pitch first exceeds interval with offset increasing with increasing pitch. Offset direction changes between climb and dive. Set to 0 to disable (Not for pixel OSD)
3700 - name: osd_home_position_arm_screen
3703 description: Should home position coordinates be displayed on the arming screen.
3704 - name: osd_pan_servo_index
3705 description: Index of the pan servo, used to adjust osd home heading direction based on camera pan. Note that this feature does not work with continiously rotating servos.
3706 field: pan_servo_index
3710 - name: osd_pan_servo_pwm2centideg
3711 description: Centidegrees of pan servo rotation us PWM signal. A servo with 180 degrees of rotation from 1000 to 2000 us PWM typically needs `18` for this setting. Change sign to inverse direction.
3712 field: pan_servo_pwm2centideg
3716 - name: osd_pan_servo_offcentre_warning
3717 description: Degrees either side of the pan servo centre; where it is assumed camera is wanted to be facing forwards, but isn't at 0. If in this range and not 0 for longer than 10 seconds, the pan servo offset OSD element will blink. 0 means the warning is disabled.
3718 field: pan_servo_offcentre_warning
3722 - name: osd_pan_servo_indicator_show_degrees
3723 description: Show the degress of offset from centre on the pan servo OSD display element.
3724 field: pan_servo_indicator_show_degrees
3727 - name: osd_esc_rpm_precision
3728 description: Number of characters used to display the RPM value.
3729 field: esc_rpm_precision
3733 - name: osd_mah_precision
3734 description: Number of digits used for mAh precision. Currently used by mAh Used and Battery Remaining Capacity
3735 field: mAh_precision
3740 - name: osd_use_pilot_logo
3741 description: Use custom pilot logo with/instead of the INAV logo. The pilot logo must be characters 473 to 511
3742 field: use_pilot_logo
3745 - name: osd_inav_to_pilot_logo_spacing
3746 description: The space between the INAV and pilot logos, if `osd_use_pilot_logo` is `ON`. This number may be adjusted so that it fits the odd/even col width displays. For example, if using an odd column width display, such as Walksnail, and this is set to 4. 1 will be added so that the logos are equally spaced from the centre of the screen.
3747 field: inav_to_pilot_logo_spacing
3751 - name: osd_arm_screen_display_time
3752 description: Amount of time to display the arm screen [ms]
3753 field: arm_screen_display_time
3757 - name: osd_system_msg_display_time
3758 description: System message display cycle time for multiple messages (milliseconds).
3759 field: system_msg_display_time
3763 - name: osd_highlight_djis_missing_font_symbols
3764 description: Show question marks where there is no symbol in the DJI font to represent the INAV OSD element's symbol. When off, blank spaces will be used. Only relevent for DJICOMPAT modes.
3765 field: highlight_djis_missing_characters
3768 - name: osd_switch_indicator_zero_name
3769 description: "Character to use for OSD switch incicator 0."
3770 field: osd_switch_indicator0_name
3773 default_value: "FLAP"
3774 - name: osd_switch_indicator_one_name
3775 description: "Character to use for OSD switch incicator 1."
3776 field: osd_switch_indicator1_name
3779 default_value: "GEAR"
3780 - name: osd_switch_indicator_two_name
3781 description: "Character to use for OSD switch incicator 2."
3782 field: osd_switch_indicator2_name
3785 default_value: "CAM"
3786 - name: osd_switch_indicator_three_name
3787 description: "Character to use for OSD switch incicator 3."
3788 field: osd_switch_indicator3_name
3791 default_value: "LIGT"
3792 - name: osd_switch_indicator_zero_channel
3793 description: "RC Channel to use for OSD switch indicator 0."
3794 field: osd_switch_indicator0_channel
3796 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3798 - name: osd_switch_indicator_one_channel
3799 description: "RC Channel to use for OSD switch indicator 1."
3800 field: osd_switch_indicator1_channel
3802 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3804 - name: osd_switch_indicator_two_channel
3805 description: "RC Channel to use for OSD switch indicator 2."
3806 field: osd_switch_indicator2_channel
3808 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3810 - name: osd_switch_indicator_three_channel
3811 description: "RC Channel to use for OSD switch indicator 3."
3812 field: osd_switch_indicator3_channel
3814 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3816 - name: osd_switch_indicators_align_left
3817 description: "Align text to left of switch indicators"
3818 field: osd_switch_indicators_align_left
3821 - name: PG_OSD_COMMON_CONFIG
3822 type: osdCommonConfig_t
3823 headers: ["io/osd_common.h"]
3824 condition: USE_OSD || USE_DJI_HD_OSD
3826 - name: osd_speed_source
3827 description: "Sets the speed type displayed by the DJI OSD and OSD canvas (FrSky Pixel): GROUND, 3D, AIR"
3828 default_value: "GROUND"
3830 table: osdSpeedSource
3833 - name: PG_SYSTEM_CONFIG
3834 type: systemConfig_t
3835 headers: ["fc/config.h"]
3838 description: "This setting controls the clock speed of I2C bus. 400KHZ is the default that most setups are able to use. Some noise-free setups may be overclocked to 800KHZ. Some sensor chips or setups with long wires may work unreliably at 400KHZ - user can try lowering the clock speed to 200KHZ or even 100KHZ. User need to bear in mind that lower clock speeds might require higher looptimes (lower looptime rate)"
3839 default_value: "400KHZ"
3843 description: "Defines debug values exposed in debug variables (developer / debugging setting)"
3844 default_value: "NONE"
3846 - name: ground_test_mode
3847 description: "For developer ground test use. Disables motors, sets heading status = Trusted on FW."
3848 condition: USE_DEV_TOOLS
3850 field: groundTestMode
3852 - name: throttle_tilt_comp_str
3853 description: "Can be used in ANGLE and HORIZON mode and will automatically boost throttle when banking. Setting is in percentage, 0=disabled."
3855 field: throttle_tilt_compensation_strength
3859 description: "Craft name"
3863 max: MAX_NAME_LENGTH
3865 description: "Pilot name"
3869 max: MAX_NAME_LENGTH
3871 - name: PG_MODE_ACTIVATION_OPERATOR_CONFIG
3872 type: modeActivationOperatorConfig_t
3873 headers: ["fc/rc_modes.h"]
3875 - name: mode_range_logic_operator
3876 description: "Control how Mode selection works in flight modes. If you example have Angle mode configured on two different Aux channels, this controls if you need both activated ( AND ) or if you only need one activated ( OR ) to active angle mode."
3878 field: modeActivationOperator
3882 - name: PG_STATS_CONFIG
3884 headers: ["fc/stats.h"]
3885 condition: USE_STATS
3888 description: "General switch of the statistics recording feature (a.k.a. odometer)"
3890 field: stats_enabled
3892 - name: stats_total_time
3893 description: "Total flight time [in seconds]. The value is updated on every disarm when \"stats\" are enabled."
3896 - name: stats_total_dist
3897 description: "Total flight distance [in meters]. The value is updated on every disarm when \"stats\" are enabled."
3900 - name: stats_total_energy
3901 description: "Total energy consumption [in mWh]. The value is updated on every disarm when \"stats\" are enabled."
3906 - name: PG_TIME_CONFIG
3908 headers: ["common/time.h"]
3911 description: "Time zone offset from UTC, in minutes. This is applied to the GPS time for logging and time-stamping of Blackbox logs"
3915 - name: tz_automatic_dst
3916 description: "Automatically add Daylight Saving Time to the GPS time when needed or simply ignore it. Includes presets for EU and the USA - if you live outside these areas it is suggested to manage DST manually via `tz_offset`."
3917 default_value: "OFF"
3919 table: tz_automatic_dst
3921 - name: PG_DISPLAY_CONFIG
3922 type: displayConfig_t
3923 headers: ["drivers/display.h"]
3925 - name: display_force_sw_blink
3926 description: "OFF = OSD hardware blink / ON = OSD software blink. If OSD warning text/values are invisible, try setting this to ON"
3928 field: force_sw_blink
3931 - name: PG_VTX_CONFIG
3933 headers: ["io/vtx_control.h"]
3934 condition: USE_VTX_CONTROL
3936 - name: vtx_halfduplex
3937 description: "Use half duplex UART to communicate with the VTX, using only a TX pin in the FC."
3941 - name: vtx_smartaudio_early_akk_workaround
3942 description: "Enable workaround for early AKK SAudio-enabled VTX bug."
3944 field: smartAudioEarlyAkkWorkaroundEnable
3946 - name: vtx_smartaudio_alternate_softserial_method
3947 description: "Enable the alternate softserial method. This is the method used in INAV 3.0 and ealier."
3949 field: smartAudioAltSoftSerialMethod
3951 - name: vtx_softserial_shortstop
3952 description: "Enable the 3x shorter stopbit on softserial. Need for some IRC Tramp VTXes."
3954 field: softSerialShortStop
3956 - name: vtx_smartaudio_stopbits
3957 description: "Set stopbit count for serial (TBS Sixty9 SmartAudio 2.1 require value of 1 bit)"
3959 field: smartAudioStopBits
3963 - name: PG_VTX_SETTINGS_CONFIG
3964 type: vtxSettingsConfig_t
3965 headers: ["drivers/vtx_common.h", "io/vtx.h"]
3966 condition: USE_VTX_SMARTAUDIO || USE_VTX_TRAMP
3969 description: "Configure the VTX band. Bands: 1: A, 2: B, 3: E, 4: F, 5: Race."
3972 min: VTX_SETTINGS_MIN_BAND
3973 max: VTX_SETTINGS_MAX_BAND
3975 description: "Channel to use within the configured `vtx_band`. Valid values are [1, 8]."
3978 min: VTX_SETTINGS_MIN_CHANNEL
3979 max: VTX_SETTINGS_MAX_CHANNEL
3981 description: "VTX RF power level to use. The exact number of mw depends on the VTX hardware."
3984 min: VTX_SETTINGS_MIN_POWER
3985 max: VTX_SETTINGS_MAX_POWER
3986 - name: vtx_low_power_disarm
3987 description: "When the craft is disarmed, set the VTX to its lowest power. `ON` will set the power to its minimum value on startup, increase it to `vtx_power` when arming and change it back to its lowest setting after disarming. `UNTIL_FIRST_ARM` will start with minimum power, but once the craft is armed it will increase to `vtx_power` and it will never decrease until the craft is power cycled."
3988 default_value: "OFF"
3989 field: lowPowerDisarm
3990 table: vtx_low_power_disarm
3992 - name: vtx_pit_mode_chan
3993 description: "Pit mode channel."
3995 min: VTX_SETTINGS_MIN_CHANNEL
3996 max: VTX_SETTINGS_MAX_CHANNEL
3998 - name: vtx_max_power_override
3999 description: "Some VTXes may report max power incorrectly (i.e. 200mW for a 600mW VTX). Use this to override max supported power. 0 to disable and use whatever VTX reports as its capabilities"
4001 field: maxPowerOverride
4004 - name: vtx_frequency_group
4005 field: frequencyGroup
4006 description: "VTx Frequency group to use. Frequency groups: FREQUENCYGROUP_5G8: 5.8GHz, FREQUENCYGROUP_2G4: 2.4GHz, FREQUENCYGROUP_1G3: 1.3GHz."
4007 table: vtx_frequency_groups
4010 default_value: FREQUENCYGROUP_5G8
4012 - name: PG_PINIOBOX_CONFIG
4013 type: pinioBoxConfig_t
4014 headers: ["io/piniobox.h"]
4015 condition: USE_PINIOBOX
4018 field: permanentId[0]
4019 description: "Mode assignment for PINIO#1"
4020 default_value: "target specific"
4023 default_value: :BOX_PERMANENT_ID_NONE
4026 field: permanentId[1]
4027 default_value: "target specific"
4028 description: "Mode assignment for PINIO#1"
4031 default_value: :BOX_PERMANENT_ID_NONE
4034 field: permanentId[2]
4035 default_value: "target specific"
4036 description: "Mode assignment for PINIO#1"
4039 default_value: :BOX_PERMANENT_ID_NONE
4042 field: permanentId[3]
4043 default_value: "target specific"
4044 description: "Mode assignment for PINIO#1"
4047 default_value: :BOX_PERMANENT_ID_NONE
4050 - name: PG_LOG_CONFIG
4052 headers: ["common/log.h"]
4058 description: "Defines serial debugging log level. See `docs/development/serial_printf_debugging.md` for usage."
4059 default_value: "ERROR"
4064 description: "Defines serial debugging log topic. See `docs/development/serial_printf_debugging.md` for usage."
4067 - name: PG_ESC_SENSOR_CONFIG
4068 type: escSensorConfig_t
4069 headers: ["sensors/esc_sensor.h"]
4070 condition: USE_ESC_SENSOR
4072 - name: esc_sensor_listen_only
4074 description: "Enable when BLHeli32 Auto Telemetry function is used. Disable in every other case"
4079 - name: PG_SMARTPORT_MASTER_CONFIG
4080 type: smartportMasterConfig_t
4081 headers: ["io/smartport_master.h"]
4082 condition: USE_SMARTPORT_MASTER
4084 - name: smartport_master_halfduplex
4088 - name: smartport_master_inverted
4093 - name: PG_DJI_OSD_CONFIG
4094 type: djiOsdConfig_t
4095 headers: ["io/osd_dji_hd.h"]
4096 condition: USE_DJI_HD_OSD
4098 - name: dji_use_name_for_messages
4099 description: "Re-purpose the craft name field for messages."
4101 field: use_name_for_messages
4103 - name: dji_esc_temp_source
4104 description: "Re-purpose the ESC temperature field for IMU/BARO temperature"
4105 default_value: "ESC"
4106 field: esc_temperature_source
4107 table: djiOsdTempSource
4109 - name: dji_message_speed_source
4110 description: "Sets the speed type displayed by the DJI OSD in craft name: GROUND, 3D, AIR"
4112 field: messageSpeedSource
4113 table: osdSpeedSource
4115 - name: dji_rssi_source
4116 description: "Source of the DJI RSSI field: RSSI, CRSF_LQ"
4117 default_value: "RSSI"
4119 table: djiRssiSource
4121 - name: dji_use_adjustments
4122 description: "Show inflight adjustments in craft name field"
4125 field: useAdjustments
4126 - name: dji_cn_alternating_duration
4127 description: "Alternating duration of craft name elements, in tenths of a second"
4131 field: craftNameAlternatingDuration
4134 - name: PG_BEEPER_CONFIG
4135 type: beeperConfig_t
4136 headers: [ "fc/config.h" ]
4138 - name: dshot_beeper_enabled
4139 description: "Whether using DShot motors as beepers is enabled"
4141 field: dshot_beeper_enabled
4143 - name: dshot_beeper_tone
4144 description: "Sets the DShot beeper tone"
4148 field: dshot_beeper_tone
4150 - name: beeper_pwm_mode
4154 description: "Allows disabling PWM mode for beeper on some targets. Switch from ON to OFF if the external beeper sound is weak. Do not switch from OFF to ON without checking if the board supports PWM beeper mode"
4156 - name: PG_POWER_LIMITS_CONFIG
4157 type: powerLimitsConfig_t
4158 headers: ["flight/power_limits.h"]
4159 condition: USE_POWER_LIMITS
4162 description: "Throttle attenuation PI control P term"
4167 description: "Throttle attenuation PI control I term"
4171 - name: limit_attn_filter_cutoff
4172 description: "Throttle attenuation PI control output filter cutoff frequency"
4174 field: attnFilterCutoff
4177 - name: PG_LEDPIN_CONFIG
4178 type: ledPinConfig_t
4179 headers: ["drivers/light_ws2811strip.h"]
4181 - name: led_pin_pwm_mode
4182 condition: USE_LED_STRIP
4183 description: "PWM mode of LED pin."
4184 default_value: "SHARED_LOW"
4185 field: led_pin_pwm_mode
4186 table: led_pin_pwm_mode
4188 - name: PG_OSD_JOYSTICK_CONFIG
4189 type: osdJoystickConfig_t
4190 headers: ["io/osd_joystick.h"]
4191 condition: USE_RCDEVICE && USE_LED_STRIP
4193 - name: osd_joystick_enabled
4194 description: "Enable OSD Joystick emulation"
4196 field: osd_joystick_enabled
4198 - name: osd_joystick_down
4199 description: "PWM value for DOWN key"
4201 field: osd_joystick_down
4204 - name: osd_joystick_up
4205 description: "PWM value for UP key"
4207 field: osd_joystick_up
4210 - name: osd_joystick_left
4211 description: "PWM value for LEFT key"
4213 field: osd_joystick_left
4216 - name: osd_joystick_right
4217 description: "PWM value for RIGHT key"
4219 field: osd_joystick_right
4222 - name: osd_joystick_enter
4223 description: "PWM value for ENTER key"
4225 field: osd_joystick_enter
4229 - name: PG_FW_AUTOLAND_CONFIG
4230 type: navFwAutolandConfig_t
4231 headers: ["navigation/navigation.h"]
4232 condition: USE_FW_AUTOLAND
4234 - name: nav_fw_land_approach_length
4235 description: "Length of the final approach"
4236 default_value: 35000
4237 field: approachLength
4240 - name: nav_fw_land_final_approach_pitch2throttle_mod
4241 description: "Modifier for pitch to throttle ratio at final approach. In Percent."
4243 field: finalApproachPitchToThrottleMod
4246 - name: nav_fw_land_glide_alt
4247 description: "Initial altitude of the glide phase"
4249 field: glideAltitude
4252 - name: nav_fw_land_flare_alt
4253 description: "Initial altitude of the flare phase"
4255 field: flareAltitude
4258 - name: nav_fw_land_glide_pitch
4259 description: "Pitch value for glide phase. In degrees."
4264 - name: nav_fw_land_flare_pitch
4265 description: "Pitch value for flare phase. In degrees"
4270 - name: nav_fw_land_max_tailwind
4271 description: "Max. tailwind (in cm/s) if no landing direction with downwind is available"
4276 - name: PG_GIMBAL_CONFIG
4277 type: gimbalConfig_t
4278 headers: ["drivers/gimbal_common.h"]
4279 condition: USE_SERIAL_GIMBAL
4281 - name: gimbal_pan_channel
4282 description: "Gimbal pan rc channel index. 0 is no channel."
4287 - name: gimbal_roll_channel
4288 description: "Gimbal roll rc channel index. 0 is no channel."
4293 - name: gimbal_tilt_channel
4294 description: "Gimbal tilt rc channel index. 0 is no channel."
4299 - name: gimbal_sensitivity
4300 description: "Gimbal sensitivity is similar to gain and will affect how quickly the gimbal will react."
4305 - name: gimbal_pan_trim
4307 description: "Trim gimbal pan center position."
4311 - name: gimbal_tilt_trim
4313 description: "Trim gimbal tilt center position."
4317 - name: gimbal_roll_trim
4319 description: "Trim gimbal roll center position."
4323 - name: PG_GIMBAL_SERIAL_CONFIG
4324 type: gimbalSerialConfig_t
4325 headers: ["io/gimbal_serial.h"]
4326 condition: USE_SERIAL_GIMBAL
4328 - name: gimbal_serial_single_uart
4329 description: "Gimbal serial and headtracker device share same UART. FC RX goes to headtracker device, FC TX goes to gimbal."
4333 - name: PG_HEADTRACKER_CONFIG
4334 type: headTrackerConfig_t
4335 headers: ["drivers/headtracker_common.h"]
4336 condition: USE_HEADTRACKER
4338 - name: headtracker_type
4339 description: "Type of headtrackr dervice"
4340 default_value: "NONE"
4343 table: headtracker_dev_type
4344 - name: headtracker_pan_ratio
4345 description: "Head pan movement vs camera movement ratio"
4351 - name: headtracker_tilt_ratio
4352 description: "Head tilt movement vs camera movement ratio"
4358 - name: headtracker_roll_ratio
4359 description: "Head roll movement vs camera movement ratio"