3 values: ["DEFAULT", "CW0", "CW90", "CW180", "CW270", "CW0FLIP", "CW90FLIP", "CW180FLIP", "CW270FLIP"]
5 values: ["256HZ", "188HZ", "98HZ", "42HZ", "20HZ", "10HZ"]
7 values: ["NONE", "AUTO", "MPU6000", "MPU6500", "MPU9250", "BMI160", "ICM20689", "BMI088", "ICM42605", "BMI270","LSM6DXX", "FAKE"]
8 enum: accelerationSensor_e
9 - name: rangefinder_hardware
10 values: ["NONE", "SRF10", "VL53L0X", "MSP", "BENEWAKE", "VL53L1X", "US42", "TOF10120_I2C", "FAKE"]
11 enum: rangefinderType_e
13 values: ["NONE", "AUTO", "HMC5883", "AK8975", "MAG3110", "AK8963", "IST8310", "QMC5883", "MPU9250", "IST8308", "LIS3MDL", "MSP", "RM3100", "VCM5883", "MLX90393", "FAKE"]
15 - name: opflow_hardware
16 values: ["NONE", "CXOF", "MSP", "FAKE"]
17 enum: opticalFlowSensor_e
19 values: ["NONE", "AUTO", "BMP085", "MS5611", "BMP280", "MS5607", "LPS25H", "SPL06", "BMP388", "DPS310", "B2SMPB", "MSP", "FAKE"]
21 - name: pitot_hardware
22 values: ["NONE", "AUTO", "MS4525", "ADC", "VIRTUAL", "FAKE", "MSP", "DLVR-L10D"]
25 values: ["NONE", "SERIAL", "MSP", "SIM (SITL)"]
26 enum: rxReceiverType_e
28 values: ["SPEK1024", "SPEK2048", "SBUS", "SUMD", "IBUS", "JETIEXBUS", "CRSF", "FPORT", "SBUS_FAST", "FPORT2", "SRXL2", "GHST", "MAVLINK", "FBUS"]
29 - name: blackbox_device
30 values: ["SERIAL", "SPIFLASH", "SDCARD"]
31 - name: motor_pwm_protocol
32 values: ["STANDARD", "ONESHOT125", "MULTISHOT", "BRUSHED", "DSHOT150", "DSHOT300", "DSHOT600"]
33 - name: servo_protocol
34 values: ["PWM", "SBUS", "SBUS_PWM"]
35 - name: failsafe_procedure
36 values: ["LAND", "DROP", "RTH", "NONE"]
37 - name: current_sensor
38 values: ["NONE", "ADC", "VIRTUAL", "FAKE", "ESC"]
40 - name: voltage_sensor
41 values: ["NONE", "ADC", "ESC", "FAKE"]
43 - name: imu_inertia_comp_method
44 values: ["VELNED", "TURNRATE","ADAPTIVE"]
45 enum: imu_inertia_comp_method_e
47 values: ["UBLOX", "UBLOX7", "MSP", "FAKE"]
50 values: ["AUTO", "EGNOS", "WAAS", "MSAS", "GAGAN", "SPAN", "NONE"]
53 values: ["PEDESTRIAN","AUTOMOTIVE", "AIR_1G", "AIR_2G", "AIR_4G"]
56 values: ["NEVER", "FIRST_ARM", "EACH_ARM"]
58 values: ["RIGHT", "LEFT", "YAW"]
59 - name: nav_user_control_mode
60 values: ["ATTI", "CRUISE"]
61 - name: nav_rth_alt_mode
62 values: ["CURRENT", "EXTRA", "FIXED", "MAX", "AT_LEAST"]
63 - name: nav_rth_climb_first_stage_modes
64 values: ["AT_LEAST", "EXTRA"]
66 values: ["IMPERIAL", "METRIC", "METRIC_MPH", "UK", "GA"]
68 - name: osd_stats_energy_unit
70 enum: osd_stats_energy_unit_e
71 - name: osd_stats_min_voltage_unit
72 values: ["BATTERY", "CELL"]
73 enum: osd_stats_min_voltage_unit_e
74 - name: osd_video_system
75 values: ["AUTO", "PAL", "NTSC", "HDZERO", "DJIWTF", "AVATAR", "BF43COMPAT", "BFHDCOMPAT"]
78 values: ["OFF", "ON","TEST"]
81 values: ["LEFT", "RIGHT"]
84 values: ["NORMAL", "MEDIUM", "SLOW"]
86 values: ["400KHZ", "800KHZ", "100KHZ", "200KHZ"]
88 values: ["NONE", "AGL", "FLOW_RAW", "FLOW", "ALWAYS", "SAG_COMP_VOLTAGE",
89 "VIBE", "CRUISE", "REM_FLIGHT_TIME", "SMARTAUDIO", "ACC",
90 "NAV_YAW", "PCF8574", "DYN_GYRO_LPF", "AUTOLEVEL", "ALTITUDE",
91 "AUTOTRIM", "AUTOTUNE", "RATE_DYNAMICS", "LANDING", "POS_EST"]
94 enum: modeActivationOperator_e
95 - name: osd_crosshairs_style
96 values: ["DEFAULT", "AIRCRAFT", "TYPE3", "TYPE4", "TYPE5", "TYPE6", "TYPE7", "TYPE8"]
97 enum: osd_crosshairs_style_e
98 - name: osd_sidebar_scroll
99 values: ["NONE", "ALTITUDE", "SPEED", "HOME_DISTANCE"]
100 enum: osd_sidebar_scroll_e
101 - name: nav_rth_allow_landing
102 values: ["NEVER", "ALWAYS", "FS_ONLY"]
103 enum: navRTHAllowLanding_e
104 - name: bat_capacity_unit
105 values: ["MAH", "MWH"]
106 enum: batCapacityUnit_e
107 - name: bat_voltage_source
108 values: ["RAW", "SAG_COMP"]
109 enum: batVoltageSource_e
110 - name: smartport_fuel_unit
111 values: ["PERCENT", "MAH", "MWH"]
112 enum: smartportFuelUnit_e
113 - name: platform_type
114 values: ["MULTIROTOR", "AIRPLANE", "HELICOPTER", "TRICOPTER", "ROVER", "BOAT"]
115 - name: tz_automatic_dst
116 values: ["OFF", "EU", "USA"]
117 enum: tz_automatic_dst_e
118 - name: vtx_low_power_disarm
119 values: ["OFF", "ON", "UNTIL_FIRST_ARM"]
120 enum: vtxLowerPowerDisarm_e
121 - name: vtx_frequency_groups
122 values: ["FREQUENCYGROUP_5G8", "FREQUENCYGROUP_2G4", "FREQUENCYGROUP_1G3"]
123 enum: vtxFrequencyGroups_e
125 values: ["PT1", "BIQUAD"]
126 - name: filter_type_full
127 values: ["PT1", "BIQUAD", "PT2", "PT3"]
129 values: ["ERROR", "WARNING", "INFO", "VERBOSE", "DEBUG"]
131 values: ["OFF", "RP", "RPY"]
133 - name: airmodeHandlingType
134 values: ["STICK_CENTER", "THROTTLE_THRESHOLD", "STICK_CENTER_ONCE"]
135 - name: nav_extra_arming_safety
136 values: ["ON", "ALLOW_BYPASS"]
137 enum: navExtraArmingSafety_e
139 values: ["NONE", "AUTO", "ADC", "CHANNEL", "PROTOCOL", "MSP"]
142 values: ["NONE", "PID", "PIFF", "AUTO"]
144 - name: osd_ahi_style
145 values: ["DEFAULT", "LINE"]
146 enum: osd_ahi_style_e
149 values: ["AUTO", "ON", "OFF"]
150 - name: osd_crsf_lq_format
151 enum: osd_crsf_lq_format_e
152 values: ["TYPE1", "TYPE2", "TYPE3"]
154 values: ["OFF", "ON"]
155 - name: djiOsdTempSource
156 values: ["ESC", "IMU", "BARO"]
157 enum: djiOsdTempSource_e
158 - name: osdSpeedSource
159 values: ["GROUND", "3D", "AIR"]
160 enum: osdSpeedSource_e
161 - name: nav_overrides_motor_stop
162 enum: navOverridesMotorStop_e
163 values: ["OFF_ALWAYS", "OFF", "AUTO_ONLY", "ALL_NAV"]
164 - name: osd_plus_code_short
165 values: ["0", "2", "4", "6"]
166 - name: autotune_rate_adjustment
167 enum: autotune_rate_adjustment_e
168 values: ["FIXED", "LIMIT", "AUTO"]
169 - name: safehome_usage_mode
170 values: ["OFF", "RTH", "RTH_FS"]
171 enum: safehomeUsageMode_e
172 - name: nav_rth_climb_first
173 enum: navRTHClimbFirst_e
174 values: ["OFF", "ON", "ON_FW_SPIRAL"]
175 - name: nav_wp_mission_restart
176 enum: navMissionRestart_e
177 values: ["START", "RESUME", "SWITCH"]
178 - name: djiRssiSource
179 values: ["RSSI", "CRSF_LQ"]
180 enum: djiRssiSource_e
181 - name: rth_trackback_mode
182 values: ["OFF", "ON", "FS"]
183 enum: rthTrackbackMode_e
184 - name: dynamic_gyro_notch_mode
185 values: ["2D", "3D_R", "3D_P", "3D_Y", "3D_RP", "3D_RY", "3D_PY", "3D"]
186 enum: dynamicGyroNotchMode_e
187 - name: nav_fw_wp_turn_smoothing
188 values: ["OFF", "ON", "ON-CUT"]
189 enum: wpFwTurnSmoothing_e
190 - name: gps_auto_baud_max
191 values: [ '115200', '57600', '38400', '19200', '9600', '230400', '460800', '921600']
193 - name: nav_mc_althold_throttle
194 values: ["STICK", "MID_STICK", "HOVER"]
195 enum: navMcAltHoldThrottle_e
196 - name: led_pin_pwm_mode
197 values: ["SHARED_LOW", "SHARED_HIGH", "LOW", "HIGH"]
198 enum: led_pin_pwm_mode_e
207 ROLL_PITCH_RATE_MIN: 4
208 ROLL_PITCH_RATE_MAX: 180
210 MAX_CONTROL_RATE_PROFILE_COUNT: 3
211 MAX_BATTERY_PROFILE_COUNT: 3
215 - name: PG_GYRO_CONFIG
217 headers: ["sensors/gyro.h"]
220 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."
223 - name: gyro_hardware_lpf
224 description: "Hardware lowpass filter for gyro. This value should never be changed without a very strong reason! If you have to set gyro lpf below 256HZ, it means the frame is vibrating too much, and that should be fixed first."
225 default_value: "256HZ"
228 - name: gyro_anti_aliasing_lpf_hz
229 description: "Gyro processing anti-aliasing filter cutoff frequency. In normal operation this filter setting should never be changed. In Hz"
231 field: gyro_anti_aliasing_lpf_hz
233 - name: gyro_anti_aliasing_lpf_type
234 description: "Specifies the type of the software LPF of the gyro signals."
236 field: gyro_anti_aliasing_lpf_type
238 - name: gyro_main_lpf_hz
239 description: "Software based gyro main lowpass filter. Value is cutoff frequency (Hz)"
241 field: gyro_main_lpf_hz
244 - name: gyro_main_lpf_type
245 description: "Defines the type of the main gyro LPF filter. Possible values: `PT1`, `BIQUAD`. `PT1` offers faster filter response while `BIQUAD` better attenuation."
246 default_value: BIQUAD
247 field: gyro_main_lpf_type
249 - name: gyro_use_dyn_lpf
250 description: "Use Dynamic LPF instead of static gyro stage1 LPF. Dynamic Gyro LPF updates gyro LPF based on the throttle position."
254 - name: gyro_dyn_lpf_min_hz
255 description: "Minimum frequency of the gyro Dynamic LPF"
257 field: gyroDynamicLpfMinHz
260 - name: gyro_dyn_lpf_max_hz
261 description: "Maximum frequency of the gyro Dynamic LPF"
263 field: gyroDynamicLpfMaxHz
266 - name: gyro_dyn_lpf_curve_expo
267 description: "Expo value for the throttle-to-frequency mapping for Dynamic LPF"
269 field: gyroDynamicLpfCurveExpo
272 - name: dynamic_gyro_notch_enabled
273 description: "Enable/disable dynamic gyro notch also known as Matrix Filter"
275 field: dynamicGyroNotchEnabled
276 condition: USE_DYNAMIC_FILTERS
278 - name: dynamic_gyro_notch_q
279 description: "Q factor for dynamic notches"
281 field: dynamicGyroNotchQ
282 condition: USE_DYNAMIC_FILTERS
285 - name: dynamic_gyro_notch_min_hz
286 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`"
288 field: dynamicGyroNotchMinHz
289 condition: USE_DYNAMIC_FILTERS
292 - name: dynamic_gyro_notch_mode
293 description: "Gyro dynamic notch type"
295 table: dynamic_gyro_notch_mode
296 field: dynamicGyroNotchMode
297 condition: USE_DYNAMIC_FILTERS
298 - name: dynamic_gyro_notch_3d_q
299 description: "Q factor for 3D dynamic notches"
301 field: dynamicGyroNotch3dQ
302 condition: USE_DYNAMIC_FILTERS
306 condition: USE_DUAL_GYRO
310 - name: setpoint_kalman_enabled
311 description: "Enable Kalman filter on the gyro data"
313 condition: USE_GYRO_KALMAN
316 - name: setpoint_kalman_q
317 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"
320 condition: USE_GYRO_KALMAN
323 - name: init_gyro_cal
324 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."
326 field: init_gyro_cal_enabled
329 description: "Calculated gyro zero calibration of axis X"
331 field: gyro_zero_cal[X]
335 description: "Calculated gyro zero calibration of axis Y"
337 field: gyro_zero_cal[Y]
341 description: "Calculated gyro zero calibration of axis Z"
343 field: gyro_zero_cal[Z]
346 - name: ins_gravity_cmss
347 description: "Calculated 1G of Acc axis Z to use in INS"
349 field: gravity_cmss_cal
353 - name: PG_ADC_CHANNEL_CONFIG
354 type: adcChannelConfig_t
355 headers: ["fc/config.h"]
358 - name: vbat_adc_channel
359 description: "ADC channel to use for battery voltage sensor. Defaults to board VBAT input (if available). 0 = disabled"
360 default_value: :target
361 field: adcFunctionChannel[ADC_BATTERY]
364 - name: rssi_adc_channel
365 description: "ADC channel to use for analog RSSI input. Defaults to board RSSI input (if available). 0 = disabled"
366 default_value: :target
367 field: adcFunctionChannel[ADC_RSSI]
370 - name: current_adc_channel
371 description: "ADC channel to use for analog current sensor input. Defaults to board CURRENT sensor input (if available). 0 = disabled"
372 default_value: :target
373 field: adcFunctionChannel[ADC_CURRENT]
376 - name: airspeed_adc_channel
377 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"
378 default_value: :target
379 field: adcFunctionChannel[ADC_AIRSPEED]
383 - name: PG_ACCELEROMETER_CONFIG
384 type: accelerometerConfig_t
385 headers: ["sensors/acceleration.h"]
391 - name: acc_notch_cutoff
396 description: "Selection of acc hardware. See Wiki Sensor auto detect and hardware failure detection for more info"
397 default_value: "AUTO"
400 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."
405 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."
406 default_value: "BIQUAD"
407 field: acc_soft_lpf_type
410 description: "Calculated value after '6 position avanced calibration'. See Wiki page."
412 field: accZero.raw[X]
416 description: "Calculated value after '6 position avanced calibration'. See Wiki page."
418 field: accZero.raw[Y]
422 description: "Calculated value after '6 position avanced calibration'. See Wiki page."
424 field: accZero.raw[Z]
428 description: "Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page."
430 field: accGain.raw[X]
434 description: "Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page."
436 field: accGain.raw[Y]
440 description: "Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page."
442 field: accGain.raw[Z]
446 - name: PG_RANGEFINDER_CONFIG
447 type: rangefinderConfig_t
448 headers: ["sensors/rangefinder.h"]
449 condition: USE_RANGEFINDER
451 - name: rangefinder_hardware
452 table: rangefinder_hardware
453 description: "Selection of rangefinder hardware."
454 default_value: "NONE"
455 - name: rangefinder_median_filter
456 description: "3-point median filtering for rangefinder readouts"
458 field: use_median_filtering
461 - name: PG_OPFLOW_CONFIG
462 type: opticalFlowConfig_t
463 headers: ["sensors/opflow.h"]
464 condition: USE_OPFLOW
466 - name: opflow_hardware
467 description: "Selection of OPFLOW hardware."
469 table: opflow_hardware
475 description: "Optical flow module alignment (default CW0_DEG_FLIP)"
476 default_value: CW0FLIP
481 - name: PG_COMPASS_CONFIG
482 type: compassConfig_t
483 headers: ["sensors/compass.h"]
487 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."
488 default_value: "DEFAULT"
493 description: "Selection of mag hardware. See Wiki Sensor auto detect and hardware failure detection for more info"
494 default_value: "AUTO"
496 - name: mag_declination
497 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."
502 description: "Magnetometer calibration X offset. If its 0 none offset has been applied and calibration is failed."
504 field: magZero.raw[X]
508 description: "Magnetometer calibration Y offset. If its 0 none offset has been applied and calibration is failed."
510 field: magZero.raw[Y]
514 description: "Magnetometer calibration Z offset. If its 0 none offset has been applied and calibration is failed."
516 field: magZero.raw[Z]
520 description: "Magnetometer calibration X gain. If 1024, no calibration or calibration failed"
526 description: "Magnetometer calibration Y gain. If 1024, no calibration or calibration failed"
532 description: "Magnetometer calibration Z gain. If 1024, no calibration or calibration failed"
537 - name: mag_calibration_time
538 description: "Adjust how long time the Calibration of mag will last."
540 field: magCalibrationTimeLimit
544 description: "Allow to chose between built-in and external compass sensor if they are connected to separate buses. Currently only for REVO target"
545 condition: USE_DUAL_MAG
549 - name: align_mag_roll
550 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."
552 field: rollDeciDegrees
555 - name: align_mag_pitch
556 description: "Same as align_mag_roll, but for the pitch axis."
558 field: pitchDeciDegrees
561 - name: align_mag_yaw
562 description: "Same as align_mag_roll, but for the yaw axis."
564 field: yawDeciDegrees
568 - name: PG_BAROMETER_CONFIG
569 type: barometerConfig_t
570 headers: ["sensors/barometer.h"]
573 - name: baro_hardware
574 description: "Selection of baro hardware. See Wiki Sensor auto detect and hardware failure detection for more info"
575 default_value: "AUTO"
577 - name: baro_cal_tolerance
578 description: "Baro calibration tolerance in cm. The default should allow the noisiest baro to complete calibration [cm]."
580 field: baro_calibration_tolerance
584 - name: PG_PITOTMETER_CONFIG
585 type: pitotmeterConfig_t
586 headers: ["sensors/pitotmeter.h"]
589 - name: pitot_hardware
590 description: "Selection of pitot hardware."
591 default_value: "NONE"
592 table: pitot_hardware
593 - name: pitot_lpf_milli_hz
604 headers: ["rx/rx.h", "rx/spektrum.h"]
606 - name: receiver_type
607 description: "Selection of receiver (RX) type. Additional configuration of a `serialrx_provider` and a UART will be needed for `SERIAL`"
608 default_value: :target
612 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."
618 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."
624 description: "Source of RSSI input. Possible values: `NONE`, `AUTO`, `ADC`, `CHANNEL`, `PROTOCOL`, `MSP`"
625 default_value: "AUTO"
629 description: "RX channel containing the RSSI signal"
632 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
634 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)."
637 min: RSSI_VISIBLE_VALUE_MIN
638 max: RSSI_VISIBLE_VALUE_MAX
640 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."
643 min: RSSI_VISIBLE_VALUE_MIN
644 max: RSSI_VISIBLE_VALUE_MAX
645 - name: sbus_sync_interval
646 field: sbusSyncInterval
650 - name: rc_filter_lpf_hz
651 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"
653 field: rcFilterFrequency
656 - name: rc_filter_auto
657 description: "When enabled, INAV will set RC filtering based on refresh rate and smoothing factor."
661 - name: rc_filter_smoothing_factor
662 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"
663 field: autoSmoothFactor
667 - name: serialrx_provider
668 description: "When feature SERIALRX is enabled, this allows connection to several receivers which output data via digital interface resembling serial. See RX section."
669 default_value: :target
670 condition: USE_SERIAL_RX
672 - name: serialrx_inverted
673 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)."
675 condition: USE_SERIAL_RX
677 - name: spektrum_sat_bind
678 description: "0 = disabled. Used to bind the spektrum satellite to RX"
679 condition: USE_SPEKTRUM_BIND
680 min: SPEKTRUM_SAT_BIND_DISABLED
681 max: SPEKTRUM_SAT_BIND_MAX
682 default_value: :SPEKTRUM_SAT_BIND_DISABLED
683 - name: srxl2_unit_id
684 condition: USE_SERIALRX_SRXL2
688 - name: srxl2_baud_fast
689 condition: USE_SERIALRX_SRXL2
693 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."
698 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."
702 - name: serialrx_halfduplex
703 description: "Allow serial receiver to operate on UART TX pin. With some receivers will allow control and telemetry over a single wire."
704 default_value: "AUTO"
707 - name: msp_override_channels
708 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."
710 field: mspOverrideChannels
711 condition: USE_MSP_RC_OVERRIDE
715 - name: PG_BLACKBOX_CONFIG
716 type: blackboxConfig_t
717 headers: ["blackbox/blackbox.h"]
718 condition: USE_BLACKBOX
720 - name: blackbox_rate_num
721 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"
726 - name: blackbox_rate_denom
727 description: "Blackbox logging rate denominator. See blackbox_rate_num."
732 - name: blackbox_device
733 description: "Selection of where to write blackbox data"
734 default_value: :target
736 table: blackbox_device
737 - name: sdcard_detect_inverted
738 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."
739 default_value: :target
740 field: invertedCardDetection
741 condition: USE_SDCARD
744 - name: PG_MOTOR_CONFIG
746 headers: ["flight/mixer.h"]
749 description: "This is the maximum value (in us) sent to esc when armed. Default of 1850 are OK for everyone (legacy). For modern ESCs, higher values (c. 2000) may be more appropriate. If you have brushed motors, the value should be set to 2000."
755 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."
760 - name: motor_pwm_rate
761 description: "Output frequency (in Hz) for motor pins. Applies only to brushed motors. "
766 - name: motor_pwm_protocol
767 description: "Protocol that is used to send motor updates to ESCs. Possible values - STANDARD, ONESHOT125, ONESHOT42, MULTISHOT, DSHOT150, DSHOT300, DSHOT600, DSHOT1200, BRUSHED"
768 default_value: "ONESHOT125"
769 field: motorPwmProtocol
770 table: motor_pwm_protocol
772 field: motorPoleCount
773 description: "The number of motor poles. Required to compute motor RPM"
778 - name: PG_FAILSAFE_CONFIG
779 type: failsafeConfig_t
780 headers: ["flight/failsafe.h"]
782 - name: failsafe_delay
783 description: "Time in deciseconds to wait before activating failsafe when signal is lost. See [Failsafe documentation](Failsafe.md#failsafe_delay)."
787 - name: failsafe_recovery_delay
788 description: "Time in deciseconds to wait before aborting failsafe when signal is recovered. See [Failsafe documentation](Failsafe.md#failsafe_recovery_delay)."
792 - name: failsafe_off_delay
793 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)."
797 - name: failsafe_throttle_low_delay
798 description: "If failsafe activated when throttle is low for this much time - bypass failsafe and disarm, in 10th of seconds. 0 = No timeout"
802 - name: failsafe_procedure
803 description: "What failsafe procedure to initiate in Stage 2. See [Failsafe documentation](Failsafe.md#failsafe_throttle)."
804 default_value: "LAND"
805 table: failsafe_procedure
806 - name: failsafe_stick_threshold
807 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."
809 field: failsafe_stick_motion_threshold
812 - name: failsafe_fw_roll_angle
813 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"
817 - name: failsafe_fw_pitch_angle
818 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"
822 - name: failsafe_fw_yaw_rate
823 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"
827 - name: failsafe_min_distance
828 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."
832 - name: failsafe_min_distance_procedure
833 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)."
834 default_value: "DROP"
835 table: failsafe_procedure
836 - name: failsafe_mission_delay
837 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."
841 - name: failsafe_gps_fix_estimation_delay
842 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."
843 condition: USE_GPS_FIX_ESTIMATION
848 - name: PG_LIGHTS_CONFIG
850 headers: ["io/lights.h"]
851 condition: USE_LIGHTS
853 - name: failsafe_lights
854 description: "Enable or disable the lights when the `FAILSAFE` flight mode is enabled. The target needs to be compiled with `USE_LIGHTS` [ON/OFF]."
856 field: failsafe.enabled
858 - name: failsafe_lights_flash_period
859 description: "Time in milliseconds between two flashes when `failsafe_lights` is ON and `FAILSAFE` flight mode is enabled [40-65535]."
861 field: failsafe.flash_period
864 - name: failsafe_lights_flash_on_time
865 description: "Flash lights ON time in milliseconds when `failsafe_lights` is ON and `FAILSAFE` flight mode is enabled. [20-65535]."
867 field: failsafe.flash_on_time
871 - name: PG_BOARD_ALIGNMENT
872 type: boardAlignment_t
873 headers: ["sensors/boardalignment.h"]
875 - name: align_board_roll
876 description: "Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc"
878 field: rollDeciDegrees
881 - name: align_board_pitch
882 description: "Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc"
884 field: pitchDeciDegrees
887 - name: align_board_yaw
888 description: "Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc"
890 field: yawDeciDegrees
894 - name: PG_BATTERY_METERS_CONFIG
895 type: batteryMetersConfig_t
896 headers: ["sensors/battery_config_structs.h"]
898 - name: vbat_meter_type
899 description: "Vbat voltage source. Possible values: `NONE`, `ADC`, `ESC`. `ESC` required ESC telemetry enebled and running"
903 table: voltage_sensor
906 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."
907 default_value: :target
912 - name: current_meter_scale
913 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."
914 default_value: :target
918 - name: current_meter_offset
919 description: "This sets the output offset voltage of the current sensor in millivolts."
920 default_value: :target
921 field: current.offset
924 - name: current_meter_type
925 description: "ADC , VIRTUAL, NONE. The virtual current sensor, once calibrated, estimates the current value from throttle position."
928 table: current_sensor
930 - name: bat_voltage_src
931 description: "Chose between raw and sag compensated battery voltage to use for battery alarms and telemetry. Possible values are `RAW` and `SAG_COMP`"
934 table: bat_voltage_source
937 description: "Power draw at cruise throttle used for remaining flight time/distance estimation in 0.01W unit"
943 description: "Power draw at zero throttle used for remaining flight time/distance estimation in 0.01W unit"
948 - name: rth_energy_margin
949 description: "Energy margin wanted after getting home (percent of battery energy capacity). Use for the remaining flight time/distance calculation"
953 - name: thr_comp_weight
954 description: "Weight used for the throttle compensation based on battery voltage. See the [battery documentation](Battery.md#automatic-throttle-compensation-based-on-battery-voltage)"
956 field: throttle_compensation_weight
960 - name: PG_BATTERY_PROFILES
961 type: batteryProfile_t
962 headers: ["sensors/battery_config_structs.h"]
963 value_type: BATTERY_CONFIG_VALUE
966 description: "Number of cells of the battery (0 = auto-detect), see battery documentation. 7S, 9S and 11S batteries cannot be auto-detected."
972 - name: vbat_cell_detect_voltage
973 description: "Maximum voltage per cell, used for auto-detecting the number of cells of the battery in 0.01V units."
975 field: voltage.cellDetect
979 - name: vbat_max_cell_voltage
980 description: "Maximum voltage per cell in 0.01V units, default is 4.20V"
982 field: voltage.cellMax
986 - name: vbat_min_cell_voltage
987 description: "Minimum voltage per cell, this triggers battery out alarms, in 0.01V units, default is 330 (3.3V)"
989 field: voltage.cellMin
993 - name: vbat_warning_cell_voltage
994 description: "Warning voltage per cell, this triggers battery-warning alarms, in 0.01V units, default is 350 (3.5V)"
996 field: voltage.cellWarning
1000 - name: battery_capacity
1001 description: "Set the battery capacity in mAh or mWh (see `battery_capacity_unit`). Used to calculate the remaining battery capacity."
1003 field: capacity.value
1006 - name: battery_capacity_warning
1007 description: "If the remaining battery capacity goes below this threshold the beeper will emit short beeps and the relevant OSD items will blink."
1009 field: capacity.warning
1012 - name: battery_capacity_critical
1013 description: "If the remaining battery capacity goes below this threshold the battery is considered empty and the beeper will emit long beeps."
1015 field: capacity.critical
1018 - name: battery_capacity_unit
1019 description: "Unit used for `battery_capacity`, `battery_capacity_warning` and `battery_capacity_critical` [MAH/MWH] (milliAmpere hour / milliWatt hour)."
1020 default_value: "MAH"
1021 field: capacity.unit
1022 table: bat_capacity_unit
1024 - name: controlrate_profile
1025 description: "Control rate profile to switch to when the battery profile is selected, 0 to disable and keep the currently selected control rate profile"
1027 field: controlRateProfile
1029 max: MAX_CONTROL_RATE_PROFILE_COUNT
1031 - name: throttle_scale
1032 description: "Throttle scaling factor. `1` means no throttle scaling. `0.5` means throttle scaled down by 50%"
1034 field: motor.throttleScale
1037 - name: throttle_idle
1038 description: "The percentage of the throttle range (`max_throttle` - `min_command`) above `min_command` used for minimum / idle throttle."
1040 field: motor.throttleIdle
1043 - name: turtle_mode_power_factor
1044 field: motor.turtleModePowerFactor
1046 description: "Turtle mode power factor"
1047 condition: USE_DSHOT
1050 - name: failsafe_throttle
1051 description: "Throttle level used for landing when failsafe is enabled. See [Failsafe documentation](Failsafe.md#failsafe_throttle)."
1055 - name: nav_mc_hover_thr
1056 description: "Multicopter hover throttle hint for altitude controller. Should be set to approximate throttle value when drone is hovering."
1058 field: nav.mc.hover_throttle
1061 - name: nav_fw_cruise_thr
1062 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 )"
1064 field: nav.fw.cruise_throttle
1067 - name: nav_fw_min_thr
1068 description: "Minimum throttle for flying wing in GPS assisted modes"
1070 field: nav.fw.min_throttle
1073 - name: nav_fw_max_thr
1074 description: "Maximum throttle for flying wing in GPS assisted modes"
1076 field: nav.fw.max_throttle
1079 - name: nav_fw_pitch2thr
1080 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)"
1082 field: nav.fw.pitch_to_throttle
1085 - name: nav_fw_launch_thr
1086 description: "Launch throttle - throttle to be set during launch sequence (pwm units)"
1088 field: nav.fw.launch_throttle
1091 - name: nav_fw_launch_idle_thr
1092 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)"
1094 field: nav.fw.launch_idle_throttle
1097 - name: limit_cont_current
1098 description: "Continous current limit (dA), set to 0 to disable"
1099 condition: USE_POWER_LIMITS
1101 field: powerLimits.continuousCurrent
1103 - name: limit_burst_current
1104 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"
1105 condition: USE_POWER_LIMITS
1107 field: powerLimits.burstCurrent
1109 - name: limit_burst_current_time
1110 description: "Allowed current burst time (ds) during which `limit_burst_current` is allowed and after which `limit_cont_current` will be enforced"
1111 condition: USE_POWER_LIMITS
1113 field: powerLimits.burstCurrentTime
1115 - name: limit_burst_current_falldown_time
1116 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`"
1117 condition: USE_POWER_LIMITS
1119 field: powerLimits.burstCurrentFalldownTime
1121 - name: limit_cont_power
1122 description: "Continous power limit (dW), set to 0 to disable"
1123 condition: USE_POWER_LIMITS && USE_ADC
1125 field: powerLimits.continuousPower
1127 - name: limit_burst_power
1128 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"
1129 condition: USE_POWER_LIMITS && USE_ADC
1131 field: powerLimits.burstPower
1133 - name: limit_burst_power_time
1134 description: "Allowed power burst time (ds) during which `limit_burst_power` is allowed and after which `limit_cont_power` will be enforced"
1135 condition: USE_POWER_LIMITS && USE_ADC
1137 field: powerLimits.burstPowerTime
1139 - name: limit_burst_power_falldown_time
1140 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`"
1141 condition: USE_POWER_LIMITS && USE_ADC
1143 field: powerLimits.burstPowerFalldownTime
1146 - name: PG_MIXER_PROFILE
1147 type: mixerProfile_t
1148 headers: ["flight/mixer_profile.h"]
1149 value_type: MIXER_CONFIG_VALUE
1151 - name: motor_direction_inverted
1152 description: "Use if you need to inverse yaw motor direction."
1154 field: mixer_config.motorDirectionInverted
1156 - name: platform_type
1157 description: "Defines UAV platform type. Allowed values: \"MULTIROTOR\", \"AIRPLANE\", \"HELICOPTER\", \"TRICOPTER\", \"ROVER\", \"BOAT\". Currently only MULTIROTOR, AIRPLANE and TRICOPTER types are implemented"
1158 default_value: "MULTIROTOR"
1159 field: mixer_config.platformType
1161 table: platform_type
1163 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"
1165 field: mixer_config.hasFlaps
1167 - name: model_preview_type
1168 description: "ID of mixer preset applied in a Configurator. **Do not modify manually**. Used only for backup/restore reasons."
1170 field: mixer_config.appliedMixerPreset
1173 - name: motorstop_on_low
1174 description: "If enabled, motor will stop when throttle is low on this mixer_profile"
1176 field: mixer_config.motorstopOnLow
1178 - name: mixer_pid_profile_linking
1179 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."
1181 field: mixer_config.PIDProfileLinking
1183 - name: mixer_automated_switch
1184 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"
1186 field: mixer_config.automated_switch
1188 - name: mixer_switch_trans_timer
1189 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."
1191 field: mixer_config.switchTransitionTimer
1194 - name: tailsitter_orientation_offset
1195 description: "Apply a 90 deg pitch offset in sensor aliment for tailsitter flying mode"
1197 field: mixer_config.tailsitterOrientationOffset
1202 - name: PG_REVERSIBLE_MOTORS_CONFIG
1203 type: reversibleMotorsConfig_t
1205 - name: 3d_deadband_low
1206 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)"
1211 - name: 3d_deadband_high
1212 description: "High value of throttle deadband for 3D mode (when stick is in the deadband range, the value in 3d_neutral is used instead)"
1214 field: deadband_high
1218 description: "Neutral (stop) throttle value for 3D mode"
1224 - name: PG_SERVO_CONFIG
1226 headers: ["flight/servos.h"]
1228 - name: servo_protocol
1229 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)"
1230 default_value: "PWM"
1231 field: servo_protocol
1232 table: servo_protocol
1233 - name: servo_center_pulse
1234 description: "Servo midpoint"
1236 field: servoCenterPulse
1239 - name: servo_pwm_rate
1240 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."
1245 - name: servo_lpf_hz
1246 description: "Selects the servo PWM output cutoff frequency. Value is in [Hz]"
1248 field: servo_lowpass_freq
1251 - name: flaperon_throw_offset
1252 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."
1254 min: FLAPERON_THROW_MIN
1255 max: FLAPERON_THROW_MAX
1256 - name: tri_unarmed_servo
1257 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."
1260 - name: servo_autotrim_rotation_limit
1261 description: "Servo midpoints are only updated when total aircraft rotation is less than this threshold [deg/s]. Only applies when using `feature FW_AUTOTRIM`."
1266 - name: PG_CONTROL_RATE_PROFILES
1267 type: controlRateConfig_t
1268 headers: ["fc/controlrate_profile_config_struct.h"]
1269 value_type: CONTROL_RATE_VALUE
1272 description: "Throttle value when the stick is set to mid-position. Used in the throttle curve calculation."
1274 field: throttle.rcMid8
1278 description: "Throttle exposition value"
1280 field: throttle.rcExpo8
1284 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."
1286 field: throttle.dynPID
1289 - name: tpa_breakpoint
1290 description: "See tpa_rate."
1292 field: throttle.pa_breakpoint
1296 description: "Throttle PID attenuation also reduces influence on YAW for multi-rotor, Should be set to ON for tilting rotors."
1298 field: throttle.dynPID_on_YAW
1300 - name: fw_tpa_time_constant
1301 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."
1303 field: throttle.fixedWingTauMs
1307 description: "Exposition value used for the PITCH/ROLL axes by all the stabilized flights modes (all but `MANUAL`)"
1309 field: stabilized.rcExpo8
1313 description: "Exposition value used for the YAW axis by all the stabilized flights modes (all but `MANUAL`)"
1315 field: stabilized.rcYawExpo8
1318 # New rates are in dps/10. That means, Rate of 20 means 200dps of rotation speed on given axis.
1319 # Rate 180 (1800dps) is max. value gyro can measure reliably
1321 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."
1323 field: stabilized.rates[FD_ROLL]
1324 min: ROLL_PITCH_RATE_MIN
1325 max: ROLL_PITCH_RATE_MAX
1327 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."
1329 field: stabilized.rates[FD_PITCH]
1330 min: ROLL_PITCH_RATE_MIN
1331 max: ROLL_PITCH_RATE_MAX
1333 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."
1335 field: stabilized.rates[FD_YAW]
1338 - name: manual_rc_expo
1339 description: "Exposition value used for the PITCH/ROLL axes by the `MANUAL` flight mode [0-100]"
1341 field: manual.rcExpo8
1344 - name: manual_rc_yaw_expo
1345 description: "Exposition value used for the YAW axis by the `MANUAL` flight mode [0-100]"
1347 field: manual.rcYawExpo8
1350 - name: manual_roll_rate
1351 description: "Servo travel multiplier for the ROLL axis in `MANUAL` flight mode [0-100]%"
1353 field: manual.rates[FD_ROLL]
1354 min: MANUAL_RATE_MIN
1355 max: MANUAL_RATE_MAX
1356 - name: manual_pitch_rate
1357 description: "Servo travel multiplier for the PITCH axis in `MANUAL` flight mode [0-100]%"
1359 field: manual.rates[FD_PITCH]
1360 min: MANUAL_RATE_MIN
1361 max: MANUAL_RATE_MAX
1362 - name: manual_yaw_rate
1363 description: "Servo travel multiplier for the YAW axis in `MANUAL` flight mode [0-100]%"
1365 field: manual.rates[FD_YAW]
1366 min: MANUAL_RATE_MIN
1367 max: MANUAL_RATE_MAX
1368 - name: fpv_mix_degrees
1369 field: misc.fpvCamAngleDegrees
1373 - name: rate_dynamics_center_sensitivity
1374 field: rateDynamics.sensitivityCenter
1378 description: "The center stick sensitivity for Rate Dynamics"
1379 condition: USE_RATE_DYNAMICS
1380 - name: rate_dynamics_end_sensitivity
1381 field: rateDynamics.sensitivityEnd
1385 description: "The end stick sensitivity for Rate Dynamics"
1386 condition: USE_RATE_DYNAMICS
1387 - name: rate_dynamics_center_correction
1388 field: rateDynamics.correctionCenter
1392 description: "The center stick correction for Rate Dynamics"
1393 condition: USE_RATE_DYNAMICS
1394 - name: rate_dynamics_end_correction
1395 field: rateDynamics.correctionEnd
1399 description: "The end stick correction for Rate Dynamics"
1400 condition: USE_RATE_DYNAMICS
1401 - name: rate_dynamics_center_weight
1402 field: rateDynamics.weightCenter
1406 description: "The center stick weight for Rate Dynamics"
1407 condition: USE_RATE_DYNAMICS
1408 - name: rate_dynamics_end_weight
1409 field: rateDynamics.weightEnd
1413 description: "The end stick weight for Rate Dynamics"
1414 condition: USE_RATE_DYNAMICS
1416 - name: PG_SERIAL_CONFIG
1417 type: serialConfig_t
1418 headers: ["io/serial.h"]
1420 - name: reboot_character
1421 description: "Special character used to trigger reboot"
1426 - name: PG_IMU_CONFIG
1428 headers: ["flight/imu.h"]
1431 description: "Inertial Measurement Unit KP Gain for accelerometer measurements"
1436 description: "Inertial Measurement Unit KI Gain for accelerometer measurements"
1440 - name: ahrs_dcm_kp_mag
1441 description: "Inertial Measurement Unit KP Gain for compass measurements"
1445 - name: ahrs_dcm_ki_mag
1446 description: "Inertial Measurement Unit KI Gain for compass measurements"
1451 description: "If the aircraft tilt angle exceed this value the copter will refuse to arm."
1455 - name: ahrs_acc_ignore_rate
1456 description: "Total gyro rotation rate threshold [deg/s] before scaling to consider accelerometer trustworthy"
1458 field: acc_ignore_rate
1461 - name: ahrs_acc_ignore_slope
1462 description: "Half-width of the interval to gradually reduce accelerometer weight. Centered at `imu_acc_ignore_rate` (exactly 50% weight)"
1464 field: acc_ignore_slope
1467 - name: ahrs_gps_yaw_windcomp
1468 description: "Wind compensation in heading estimation from gps groundcourse(fixed wing only)"
1470 field: gps_yaw_windcomp
1472 - name: ahrs_inertia_comp_method
1473 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"
1474 default_value: ADAPTIVE
1475 field: inertia_comp_method
1476 table: imu_inertia_comp_method
1477 - name: ahrs_gps_yaw_weight
1478 description: "Arhs gps yaw weight when mag is avaliable, 0 means no gps yaw, 100 means equal weight as compass"
1480 field: gps_yaw_weight
1484 - name: PG_ARMING_CONFIG
1485 type: armingConfig_t
1487 - name: fixed_wing_auto_arm
1488 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."
1491 - name: disarm_kill_switch
1492 description: "Disarms the motors independently of throttle value. Setting to OFF reverts to the old behaviour of disarming only when the throttle is low. Only applies when arming and disarming with an AUX channel."
1495 - name: switch_disarm_delay
1496 description: "Delay before disarming when requested by switch (ms) [0-1000]"
1498 field: switchDisarmDelayMs
1501 - name: prearm_timeout
1502 description: "Duration (ms) for which Prearm being activated is valid. after this, Prearm needs to be reset. 0 means Prearm does not timeout."
1503 default_value: 10000
1504 field: prearmTimeoutMs
1508 - name: PG_GENERAL_SETTINGS
1509 headers: ["config/general_settings.h"]
1510 type: generalSettings_t
1512 - name: applied_defaults
1513 description: "Internal (configurator) hint. Should not be changed manually"
1515 field: appliedDefaults
1521 headers: ["flight/ez_tune.h"]
1522 type: ezTuneSettings_t
1523 value_type: EZ_TUNE_VALUE
1526 description: "Enables EzTune feature"
1530 - name: ez_filter_hz
1531 description: "EzTune filter cutoff frequency"
1536 - name: ez_axis_ratio
1537 description: "EzTune axis ratio"
1543 description: "EzTune response"
1549 description: "EzTune damping"
1554 - name: ez_stability
1555 description: "EzTune stability"
1560 - name: ez_aggressiveness
1561 description: "EzTune aggressiveness"
1563 field: aggressiveness
1567 description: "EzTune rate"
1573 description: "EzTune expo"
1579 - name: PG_RPM_FILTER_CONFIG
1580 headers: ["flight/rpm_filter.h"]
1581 condition: USE_RPM_FILTER
1582 type: rpmFilterConfig_t
1584 - name: rpm_gyro_filter_enabled
1585 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"
1587 field: gyro_filter_enabled
1589 - name: rpm_gyro_harmonics
1590 description: "Number of harmonic frequences to be covered by gyro RPM filter. Default value of `1` usually works just fine"
1592 field: gyro_harmonics
1596 - name: rpm_gyro_min_hz
1597 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`"
1604 description: "Q factor for gyro RPM filter. Lower values give softer, wider attenuation. Usually there is no need to change this setting"
1610 - name: PG_GPS_CONFIG
1611 headers: [ "io/gps.h" ]
1615 - name: gps_provider
1616 description: "Which GPS protocol to be used, note that UBLOX is 5Hz and UBLOX7 is 10Hz (M8N)."
1617 default_value: "UBLOX"
1621 - name: gps_sbas_mode
1622 description: "Which SBAS mode to be used"
1623 default_value: "NONE"
1625 table: gps_sbas_mode
1627 - name: gps_dyn_model
1628 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."
1629 default_value: "AIR_2G"
1631 table: gps_dyn_model
1633 - name: gps_auto_config
1634 description: "Enable automatic configuration of UBlox GPS receivers."
1638 - name: gps_auto_baud
1639 description: "Automatic configuration of GPS baudrate(The specified baudrate in configured in ports will be used) when used with UBLOX GPS"
1643 - name: gps_auto_baud_max_supported
1644 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"
1645 default_value: "230400"
1646 table: gps_auto_baud_max
1649 - name: gps_ublox_use_galileo
1650 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]."
1652 field: ubloxUseGalileo
1654 - name: gps_ublox_use_beidou
1655 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]."
1657 field: ubloxUseBeidou
1659 - name: gps_ublox_use_glonass
1660 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]."
1662 field: ubloxUseGlonass
1664 - name: gps_min_sats
1665 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."
1670 - name: gps_ublox_nav_hz
1671 description: "Navigation update rate for UBLOX7 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."
1679 - name: PG_RC_CONTROLS_CONFIG
1680 type: rcControlsConfig_t
1681 headers: ["fc/rc_controls.h"]
1684 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."
1688 - name: yaw_deadband
1689 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."
1693 - name: pos_hold_deadband
1694 description: "Stick deadband in [r/c points], applied after r/c deadband and expo. Used for adjustments in navigation modes."
1698 - name: control_deadband
1699 description: "Stick deadband in [r/c points], applied after r/c deadband and expo. Used to check if sticks are centered."
1703 - name: alt_hold_deadband
1704 description: "Defines the deadband of throttle during alt_hold [r/c points]"
1708 - name: 3d_deadband_throttle
1709 description: "Throttle signal will be held to a fixed value when throttle is centered with an error margin defined in this parameter."
1711 field: mid_throttle_deadband
1714 - name: airmode_type
1715 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."
1716 default_value: "STICK_CENTER"
1717 field: airmodeHandlingType
1718 table: airmodeHandlingType
1719 - name: airmode_throttle_threshold
1720 description: "Defines airmode THROTTLE activation threshold when `airmode_type` **THROTTLE_THRESHOLD** is used"
1722 field: airmodeThrottleThreshold
1726 - name: PG_PID_PROFILE
1728 headers: ["flight/pid.h"]
1729 value_type: PROFILE_VALUE
1732 description: "Multicopter rate stabilisation P-gain for PITCH"
1734 field: bank_mc.pid[PID_PITCH].P
1738 description: "Multicopter rate stabilisation I-gain for PITCH"
1740 field: bank_mc.pid[PID_PITCH].I
1744 description: "Multicopter rate stabilisation D-gain for PITCH"
1746 field: bank_mc.pid[PID_PITCH].D
1750 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."
1752 field: bank_mc.pid[PID_PITCH].FF
1756 description: "Multicopter rate stabilisation P-gain for ROLL"
1758 field: bank_mc.pid[PID_ROLL].P
1762 description: "Multicopter rate stabilisation I-gain for ROLL"
1764 field: bank_mc.pid[PID_ROLL].I
1768 description: "Multicopter rate stabilisation D-gain for ROLL"
1770 field: bank_mc.pid[PID_ROLL].D
1774 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."
1776 field: bank_mc.pid[PID_ROLL].FF
1780 description: "Multicopter rate stabilisation P-gain for YAW"
1782 field: bank_mc.pid[PID_YAW].P
1786 description: "Multicopter rate stabilisation I-gain for YAW"
1788 field: bank_mc.pid[PID_YAW].I
1792 description: "Multicopter rate stabilisation D-gain for YAW"
1794 field: bank_mc.pid[PID_YAW].D
1798 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."
1800 field: bank_mc.pid[PID_YAW].FF
1804 description: "Multicopter attitude stabilisation P-gain"
1806 field: bank_mc.pid[PID_LEVEL].P
1810 description: "Multicopter attitude stabilisation low-pass filter cutoff"
1812 field: bank_mc.pid[PID_LEVEL].I
1816 description: "Multicopter attitude stabilisation HORIZON transition point"
1818 field: bank_mc.pid[PID_LEVEL].D
1822 description: "Fixed-wing rate stabilisation P-gain for PITCH"
1824 field: bank_fw.pid[PID_PITCH].P
1828 description: "Fixed-wing rate stabilisation I-gain for PITCH"
1830 field: bank_fw.pid[PID_PITCH].I
1834 description: "Fixed wing rate stabilisation D-gain for PITCH"
1836 field: bank_fw.pid[PID_PITCH].D
1840 description: "Fixed-wing rate stabilisation FF-gain for PITCH"
1842 field: bank_fw.pid[PID_PITCH].FF
1846 description: "Fixed-wing rate stabilisation P-gain for ROLL"
1848 field: bank_fw.pid[PID_ROLL].P
1852 description: "Fixed-wing rate stabilisation I-gain for ROLL"
1854 field: bank_fw.pid[PID_ROLL].I
1858 description: "Fixed wing rate stabilisation D-gain for ROLL"
1860 field: bank_fw.pid[PID_ROLL].D
1864 description: "Fixed-wing rate stabilisation FF-gain for ROLL"
1866 field: bank_fw.pid[PID_ROLL].FF
1870 description: "Fixed-wing rate stabilisation P-gain for YAW"
1872 field: bank_fw.pid[PID_YAW].P
1876 description: "Fixed-wing rate stabilisation I-gain for YAW"
1878 field: bank_fw.pid[PID_YAW].I
1882 description: "Fixed wing rate stabilisation D-gain for YAW"
1884 field: bank_fw.pid[PID_YAW].D
1888 description: "Fixed-wing rate stabilisation FF-gain for YAW"
1890 field: bank_fw.pid[PID_YAW].FF
1894 description: "Fixed-wing attitude stabilisation P-gain"
1896 field: bank_fw.pid[PID_LEVEL].P
1900 description: "Fixed-wing attitude stabilisation low-pass filter cutoff"
1902 field: bank_fw.pid[PID_LEVEL].I
1906 description: "Fixed-wing attitude stabilisation HORIZON transition point"
1908 field: bank_fw.pid[PID_LEVEL].D
1911 - name: max_angle_inclination_rll
1912 description: "Maximum inclination in level (angle) mode (ROLL axis). 100=10°"
1914 field: max_angle_inclination[FD_ROLL]
1917 - name: max_angle_inclination_pit
1918 description: "Maximum inclination in level (angle) mode (PITCH axis). 100=10°"
1920 field: max_angle_inclination[FD_PITCH]
1923 - name: dterm_lpf_hz
1924 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"
1928 - name: dterm_lpf_type
1929 description: "Defines the type of stage 1 D-term LPF filter. Possible values: `PT1`, `BIQUAD`, `PT2`, `PT3`."
1930 default_value: "PT2"
1931 field: dterm_lpf_type
1932 table: filter_type_full
1934 description: "Yaw P term low pass filter cutoff frequency. Should be disabled (set to `0`) on small multirotors (7 inches and below)"
1938 - name: fw_reference_airspeed
1939 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."
1941 field: fixedWingReferenceAirspeed
1944 - name: fw_turn_assist_yaw_gain
1945 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"
1947 field: fixedWingCoordinatedYawGain
1950 - name: fw_turn_assist_pitch_gain
1951 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"
1953 field: fixedWingCoordinatedPitchGain
1956 - name: fw_iterm_limit_stick_position
1957 description: "Iterm is not allowed to grow when stick position is above threshold. This solves the problem of bounceback or followthrough when full stick deflection is applied on poorely tuned fixed wings. In other words, stabilization is partialy disabled when pilot is actively controlling the aircraft and active when sticks are not touched. `0` mean stick is in center position, `1` means it is fully deflected to either side"
1959 field: fixedWingItermLimitOnStickPosition
1962 - name: fw_yaw_iterm_freeze_bank_angle
1963 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."
1965 field: fixedWingYawItermBankFreeze
1968 - name: pidsum_limit
1969 description: "A limitation to overall amount of correction Flight PID can request on each axis (Roll/Pitch). If when doing a hard maneuver on one axis machine looses orientation on other axis - reducing this parameter may help"
1972 min: PID_SUM_LIMIT_MIN
1973 max: PID_SUM_LIMIT_MAX
1974 - name: pidsum_limit_yaw
1975 description: "A limitation to overall amount of correction Flight PID can request on each axis (Yaw). If when doing a hard maneuver on one axis machine looses orientation on other axis - reducing this parameter may help"
1977 field: pidSumLimitYaw
1978 min: PID_SUM_LIMIT_MIN
1979 max: PID_SUM_LIMIT_MAX
1980 - name: iterm_windup
1981 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)"
1983 field: itermWindupPointPercent
1986 - name: pid_iterm_limit_percent
1987 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."
1989 field: pidItermLimitPercent
1992 - name: rate_accel_limit_roll_pitch
1993 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."
1995 field: axisAccelerationLimitRollPitch
1997 - name: rate_accel_limit_yaw
1998 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."
1999 default_value: 10000
2000 field: axisAccelerationLimitYaw
2002 - name: heading_hold_rate_limit
2003 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."
2004 min: HEADING_HOLD_RATE_LIMIT_MIN
2005 max: HEADING_HOLD_RATE_LIMIT_MAX
2007 - name: nav_mc_pos_z_p
2008 description: "P gain of altitude PID controller (Multirotor)"
2009 field: bank_mc.pid[PID_POS_Z].P
2013 - name: nav_mc_vel_z_p
2014 description: "P gain of velocity PID controller"
2015 field: bank_mc.pid[PID_VEL_Z].P
2019 - name: nav_mc_vel_z_i
2020 description: "I gain of velocity PID controller"
2021 field: bank_mc.pid[PID_VEL_Z].I
2025 - name: nav_mc_vel_z_d
2026 description: "D gain of velocity PID controller"
2027 field: bank_mc.pid[PID_VEL_Z].D
2031 - name: nav_mc_pos_xy_p
2032 description: "Controls how fast the drone will fly towards the target position. This is a multiplier to convert displacement to target velocity"
2033 field: bank_mc.pid[PID_POS_XY].P
2037 - name: nav_mc_vel_xy_p
2038 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"
2039 field: bank_mc.pid[PID_VEL_XY].P
2043 - name: nav_mc_vel_xy_i
2044 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"
2045 field: bank_mc.pid[PID_VEL_XY].I
2049 - name: nav_mc_vel_xy_d
2050 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."
2051 field: bank_mc.pid[PID_VEL_XY].D
2055 - name: nav_mc_vel_xy_ff
2056 field: bank_mc.pid[PID_VEL_XY].FF
2060 - name: nav_mc_heading_p
2061 description: "P gain of Heading Hold controller (Multirotor)"
2063 field: bank_mc.pid[PID_HEADING].P
2066 - name: nav_mc_vel_xy_dterm_lpf_hz
2067 field: navVelXyDTermLpfHz
2071 - name: nav_mc_vel_xy_dterm_attenuation
2072 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."
2073 field: navVelXyDtermAttenuation
2077 - name: nav_mc_vel_xy_dterm_attenuation_start
2078 description: "A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation begins"
2080 field: navVelXyDtermAttenuationStart
2083 - name: nav_mc_vel_xy_dterm_attenuation_end
2084 description: "A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation reaches maximum"
2086 field: navVelXyDtermAttenuationEnd
2089 - name: nav_fw_pos_z_p
2090 description: "P gain of altitude PID controller (Fixedwing)"
2092 field: bank_fw.pid[PID_POS_Z].P
2095 - name: nav_fw_pos_z_i
2096 description: "I gain of altitude PID controller (Fixedwing)"
2098 field: bank_fw.pid[PID_POS_Z].I
2101 - name: nav_fw_pos_z_d
2102 description: "D gain of altitude PID controller (Fixedwing)"
2104 field: bank_fw.pid[PID_POS_Z].D
2107 - name: nav_fw_alt_control_response
2108 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."
2110 field: fwAltControlResponseFactor
2113 - name: nav_fw_pos_xy_p
2114 description: "P gain of 2D trajectory PID controller. Play with this to get a straight line between waypoints or a straight RTH"
2116 field: bank_fw.pid[PID_POS_XY].P
2119 - name: nav_fw_pos_xy_i
2120 description: "I gain of 2D trajectory PID controller. Too high and there will be overshoot in trajectory. Better start tuning with zero"
2122 field: bank_fw.pid[PID_POS_XY].I
2125 - name: nav_fw_pos_xy_d
2126 description: "D gain of 2D trajectory PID controller. Too high and there will be overshoot in trajectory. Better start tuning with zero"
2128 field: bank_fw.pid[PID_POS_XY].D
2131 - name: nav_fw_heading_p
2132 description: "P gain of Heading Hold controller (Fixedwing)"
2134 field: bank_fw.pid[PID_HEADING].P
2137 - name: nav_fw_pos_hdg_p
2138 description: "P gain of heading PID controller. (Fixedwing, rovers, boats)"
2140 field: bank_fw.pid[PID_POS_HEADING].P
2143 - name: nav_fw_pos_hdg_i
2144 description: "I gain of heading trajectory PID controller. (Fixedwing, rovers, boats)"
2146 field: bank_fw.pid[PID_POS_HEADING].I
2149 - name: nav_fw_pos_hdg_d
2150 description: "D gain of heading trajectory PID controller. (Fixedwing, rovers, boats)"
2152 field: bank_fw.pid[PID_POS_HEADING].D
2155 - name: nav_fw_pos_hdg_pidsum_limit
2156 description: "Output limit for heading trajectory PID controller. (Fixedwing, rovers, boats)"
2158 field: navFwPosHdgPidsumLimit
2159 min: PID_SUM_LIMIT_MIN
2160 max: PID_SUM_LIMIT_MAX
2161 - name: mc_iterm_relax
2165 - name: mc_iterm_relax_cutoff
2166 field: iterm_relax_cutoff
2172 condition: USE_D_BOOST
2178 condition: USE_D_BOOST
2182 - name: d_boost_max_at_acceleration
2183 field: dBoostMaxAtAlleceleration
2184 condition: USE_D_BOOST
2188 - name: d_boost_gyro_delta_lpf_hz
2189 field: dBoostGyroDeltaLpfHz
2190 condition: USE_D_BOOST
2194 - name: antigravity_gain
2195 description: "Max Antigravity gain. `1` means Antigravity is disabled, `2` means Iterm is allowed to double during rapid throttle movements"
2197 field: antigravityGain
2198 condition: USE_ANTIGRAVITY
2201 - name: antigravity_accelerator
2204 field: antigravityAccelerator
2205 condition: USE_ANTIGRAVITY
2208 - name: antigravity_cutoff_lpf_hz
2209 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"
2211 field: antigravityCutoff
2212 condition: USE_ANTIGRAVITY
2216 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`"
2217 field: pidControllerType
2220 - name: mc_cd_lpf_hz
2221 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."
2223 field: controlDerivativeLpfHz
2226 - name: fw_level_pitch_trim
2227 description: "Pitch trim for self-leveling flight modes. In degrees. +5 means airplane nose should be raised 5 deg from level"
2229 field: fixedWingLevelTrim
2232 - name: smith_predictor_strength
2233 description: "The strength factor of a Smith Predictor of PID measurement. In percents"
2235 field: smithPredictorStrength
2236 condition: USE_SMITH_PREDICTOR
2239 - name: smith_predictor_delay
2240 description: "Expected delay of the gyro signal. In milliseconds"
2242 field: smithPredictorDelay
2243 condition: USE_SMITH_PREDICTOR
2246 - name: smith_predictor_lpf_hz
2247 description: "Cutoff frequency for the Smith Predictor Low Pass Filter"
2249 field: smithPredictorFilterHz
2250 condition: USE_SMITH_PREDICTOR
2253 - name: fw_level_pitch_gain
2254 description: "I-gain for the pitch trim for self-leveling flight modes. Higher values means that AUTOTRIM will be faster but might introduce oscillations"
2256 field: fixedWingLevelTrimGain
2260 - name: PG_PID_AUTOTUNE_CONFIG
2261 type: pidAutotuneConfig_t
2262 condition: USE_AUTOTUNE_FIXED_WING
2264 - name: fw_autotune_min_stick
2265 description: "Minimum stick input [%], after applying deadband and expo, to start recording the plane's response to stick input."
2270 - name: fw_autotune_rate_adjustment
2271 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."
2272 default_value: "AUTO"
2273 field: fw_rate_adjustment
2274 table: autotune_rate_adjustment
2276 - name: fw_autotune_max_rate_deflection
2277 description: "The target percentage of maximum mixer output used for determining the rates in `AUTO` and `LIMIT`."
2279 field: fw_max_rate_deflection
2283 - name: PG_POSITION_ESTIMATION_CONFIG
2284 type: positionEstimationConfig_t
2286 - name: inav_auto_mag_decl
2287 description: "Automatic setting of magnetic declination based on GPS position. When used manual magnetic declination is ignored."
2289 field: automatic_mag_declination
2291 - name: inav_gravity_cal_tolerance
2292 description: "Unarmed gravity calibration tolerance level. Won't finish the calibration until estimated gravity error falls below this value."
2294 field: gravity_calibration_tolerance
2297 - name: inav_use_gps_velned
2298 description: "Defined if INAV should use velocity data provided by GPS module for doing position and speed estimation. If set to OFF INAV will fallback to calculating velocity from GPS coordinates. Using native velocity data may improve performance on some GPS modules. Some GPS modules introduce significant delay and using native velocity may actually result in much worse performance."
2300 field: use_gps_velned
2302 - name: inav_use_gps_no_baro
2303 field: use_gps_no_baro
2306 - name: inav_allow_dead_reckoning
2307 description: "Defines if INAV will dead-reckon over short GPS outages. May also be useful for indoors OPFLOW navigation"
2309 field: allow_dead_reckoning
2311 - name: inav_allow_gps_fix_estimation
2312 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."
2313 condition: USE_GPS_FIX_ESTIMATION
2315 field: allow_gps_fix_estimation
2317 - name: inav_reset_altitude
2318 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)"
2319 default_value: "FIRST_ARM"
2320 field: reset_altitude_type
2322 - name: inav_reset_home
2323 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"
2324 default_value: "FIRST_ARM"
2325 field: reset_home_type
2327 - name: inav_max_surface_altitude
2328 description: "Max allowed altitude for surface following mode. [cm]"
2330 field: max_surface_altitude
2333 - name: inav_w_z_surface_p
2334 field: w_z_surface_p
2338 - name: inav_w_z_surface_v
2339 field: w_z_surface_v
2343 - name: inav_w_xy_flow_p
2348 - name: inav_w_xy_flow_v
2353 - name: inav_w_z_baro_p
2354 description: "Weight of barometer measurements in estimated altitude and climb rate. Setting is used on both airplanes and multirotors."
2359 - name: inav_w_z_gps_p
2360 description: "Weight of GPS altitude measurements in estimated altitude. Setting is used on both airplanes and multirotors."
2365 - name: inav_w_z_gps_v
2366 description: "Weight of GPS climb rate measurements in estimated climb rate. Setting is used on both airplanes and multirotors."
2371 - name: inav_w_xy_gps_p
2372 description: "Weight of GPS coordinates in estimated UAV position and speed."
2377 - name: inav_w_xy_gps_v
2378 description: "Weight of GPS velocity data in estimated UAV speed"
2383 - name: inav_w_z_res_v
2384 description: "Decay coefficient for estimated climb rate when baro/GPS reference for altitude is lost"
2389 - name: inav_w_xy_res_v
2390 description: "Decay coefficient for estimated velocity when GPS reference for position is lost"
2395 - name: inav_w_acc_bias
2396 description: "Weight for accelerometer drift estimation"
2401 - name: inav_max_eph_epv
2402 description: "Maximum uncertainty value until estimated position is considered valid and is used for navigation [cm]"
2407 - name: inav_baro_epv
2408 description: "Uncertainty value for barometric sensor [cm]"
2414 - name: PG_NAV_CONFIG
2416 headers: ["navigation/navigation.h"]
2418 - name: nav_disarm_on_landing
2419 description: "If set to ON, INAV disarms the FC after landing"
2421 field: general.flags.disarm_on_landing
2423 - name: nav_land_detect_sensitivity
2424 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."
2426 field: general.land_detect_sensitivity
2429 - name: nav_landing_bump_detection
2430 description: "Allows immediate landing detection based on G bump at touchdown when set to ON. Requires a barometer and currently only works for multirotors."
2432 field: general.flags.landing_bump_detection
2434 - name: nav_mc_althold_throttle
2435 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."
2436 default_value: "STICK"
2437 field: mc.althold_throttle_type
2438 table: nav_mc_althold_throttle
2439 - name: nav_extra_arming_safety
2440 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"
2441 default_value: "ALLOW_BYPASS"
2442 field: general.flags.extra_arming_safety
2443 table: nav_extra_arming_safety
2444 - name: nav_user_control_mode
2445 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."
2446 default_value: "ATTI"
2447 field: general.flags.user_control_mode
2448 table: nav_user_control_mode
2449 - name: nav_position_timeout
2450 description: "If GPS fails wait for this much seconds before switching to emergency landing mode (0 - disable)"
2452 field: general.pos_failure_timeout
2455 - name: nav_wp_load_on_boot
2456 description: "If set to ON, waypoints will be automatically loaded from EEPROM to the FC during startup."
2458 field: general.waypoint_load_on_boot
2460 - name: nav_wp_radius
2461 description: "Waypoint radius [cm]. Waypoint would be considered reached if machine is within this radius"
2463 field: general.waypoint_radius
2466 - name: nav_wp_enforce_altitude
2467 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."
2469 field: general.waypoint_enforce_altitude
2472 - name: nav_wp_max_safe_distance
2473 description: "First waypoint in the mission should be closer than this value [m]. A value of 0 disables this check."
2475 field: general.waypoint_safe_distance
2478 - name: nav_wp_mission_restart
2479 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."
2480 default_value: "RESUME"
2481 field: general.flags.waypoint_mission_restart
2482 table: nav_wp_mission_restart
2483 - name: nav_wp_multi_mission_index
2484 description: "Index of active mission selected from multi mission WP entry loaded in flight controller. Limited to a maximum of 9 missions."
2486 field: general.waypoint_multi_mission_index
2487 condition: USE_MULTI_MISSION
2490 - name: nav_fw_wp_tracking_accuracy
2491 description: "Waypoint tracking accuracy forces the craft to quickly head toward and track along the waypoint course line as closely as possible. Settings 1 to 10 adjust the course tracking response. Higher values dampen the response reducing possible overshoot. A value of 5 is a good starting point. Set to 0 to disable."
2493 field: fw.wp_tracking_accuracy
2496 - name: nav_fw_wp_tracking_max_angle
2497 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."
2499 field: fw.wp_tracking_max_angle
2502 - name: nav_fw_wp_turn_smoothing
2503 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)."
2504 default_value: "OFF"
2505 field: fw.wp_turn_smoothing
2506 table: nav_fw_wp_turn_smoothing
2507 - name: nav_auto_speed
2508 description: "Speed in fully autonomous modes (RTH, WP) [cm/s]. Used for WP mode when no specific WP speed set. [Multirotor only]"
2510 field: general.auto_speed
2513 - name: nav_min_ground_speed
2514 description: "Minimum ground speed for navigation flight modes [m/s]. Default 7 m/s."
2516 field: general.min_ground_speed
2519 - name: nav_max_auto_speed
2520 description: "Maximum speed allowed in fully autonomous modes (RTH, WP) [cm/s] [Multirotor only]"
2522 field: general.max_auto_speed
2525 - name: nav_manual_speed
2526 description: "Maximum speed allowed when processing pilot input for POSHOLD/CRUISE control mode [cm/s] [Multirotor only]"
2528 field: general.max_manual_speed
2531 - name: nav_land_minalt_vspd
2532 description: "Vertical descent velocity under nav_land_slowdown_minalt during the RTH landing phase. [cm/s]"
2534 field: general.land_minalt_vspd
2537 - name: nav_land_maxalt_vspd
2538 description: "Vertical descent velocity above nav_land_slowdown_maxalt during the RTH landing phase. [cm/s]"
2540 field: general.land_maxalt_vspd
2543 - name: nav_land_slowdown_minalt
2544 description: "Defines at what altitude the descent velocity should start to be `nav_land_minalt_vspd` [cm]"
2546 field: general.land_slowdown_minalt
2549 - name: nav_land_slowdown_maxalt
2550 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]"
2552 field: general.land_slowdown_maxalt
2555 - name: nav_emerg_landing_speed
2556 description: "Rate of descent UAV will try to maintain when doing emergency descent sequence [cm/s]"
2558 field: general.emerg_descent_rate
2561 - name: nav_min_rth_distance
2562 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."
2564 field: general.min_rth_distance
2567 - name: nav_overrides_motor_stop
2568 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"
2569 default_value: "ALL_NAV"
2570 field: general.flags.nav_overrides_motor_stop
2571 table: nav_overrides_motor_stop
2572 - name: nav_fw_soaring_motor_stop
2573 description: "Stops motor when Soaring mode enabled."
2575 field: general.flags.soaring_motor_stop
2577 - name: nav_fw_soaring_pitch_deadband
2578 description: "Pitch Angle deadband when soaring mode enabled (deg). Angle mode inactive within deadband allowing pitch to free float whilst soaring."
2580 field: fw.soaring_pitch_deadband
2583 - name: nav_rth_climb_first
2584 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)"
2586 field: general.flags.rth_climb_first
2587 table: nav_rth_climb_first
2588 - name: nav_rth_climb_first_stage_mode
2589 description: "This determines how rth_climb_first_stage_altitude is used. Default is AT_LEAST."
2590 default_value: "AT_LEAST"
2591 field: general.flags.rth_climb_first_stage_mode
2592 table: nav_rth_climb_first_stage_modes
2593 - name: nav_rth_climb_first_stage_altitude
2594 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."
2596 field: general.rth_climb_first_stage_altitude
2598 - name: nav_rth_climb_ignore_emerg
2599 description: "If set to ON, aircraft will execute initial climb regardless of position sensor (GPS) status."
2601 field: general.flags.rth_climb_ignore_emerg
2603 - name: nav_rth_tail_first
2604 description: "If set to ON drone will return tail-first. Obviously meaningless for airplanes."
2606 field: general.flags.rth_tail_first
2608 - name: nav_rth_allow_landing
2609 description: "If set to ON drone will land as a last phase of RTH."
2610 default_value: "ALWAYS"
2611 field: general.flags.rth_allow_landing
2612 table: nav_rth_allow_landing
2613 - name: nav_rth_fs_landing_delay
2614 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]"
2618 field: general.rth_fs_landing_delay
2619 - name: nav_rth_alt_mode
2620 description: "Configure how the aircraft will manage altitude on the way home, see Navigation modes on wiki for more details"
2621 default_value: "AT_LEAST"
2622 field: general.flags.rth_alt_control_mode
2623 table: nav_rth_alt_mode
2624 - name: nav_rth_alt_control_override
2625 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)"
2627 field: general.flags.rth_alt_control_override
2629 - name: nav_rth_abort_threshold
2630 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]"
2631 default_value: 50000
2632 field: general.rth_abort_threshold
2635 - name: nav_max_terrain_follow_alt
2636 field: general.max_terrain_follow_altitude
2637 default_value: "100"
2638 description: "Max allowed above the ground altitude for terrain following mode"
2641 - name: nav_max_altitude
2642 field: general.max_altitude
2643 description: "Max allowed altitude (above Home Point) that applies to all NAV modes (including Altitude Hold). 0 means limit is disabled"
2647 - name: nav_rth_altitude
2648 description: "Used in EXTRA, FIXED and AT_LEAST rth alt modes [cm] (Default 1000 means 10 meters)"
2650 field: general.rth_altitude
2652 - name: nav_rth_home_altitude
2653 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]"
2655 field: general.rth_home_altitude
2657 - name: nav_rth_linear_descent_start_distance
2658 description: The distance [m] away from home to start the linear descent. 0 = immediately (original linear descent behaviour)
2662 field: general.rth_linear_descent_start_distance
2663 - name: nav_rth_use_linear_descent
2664 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`.
2667 field: general.flags.rth_use_linear_descent
2668 - name: nav_rth_trackback_mode
2669 description: "Useage modes for RTH Trackback. OFF = disabled, ON = Normal and Failsafe RTH, FS = Failsafe RTH only."
2670 default_value: "OFF"
2671 field: general.flags.rth_trackback_mode
2672 table: rth_trackback_mode
2673 - name: nav_rth_trackback_distance
2674 description: "Maximum distance allowed for RTH trackback. Normal RTH is executed once this distance is exceeded [m]."
2676 field: general.rth_trackback_distance
2679 - name: safehome_max_distance
2680 description: "In order for a safehome to be used, it must be less than this distance (in cm) from the arming point."
2681 default_value: 20000
2682 field: general.safehome_max_distance
2685 - name: safehome_usage_mode
2686 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."
2687 default_value: "RTH"
2688 field: general.flags.safehome_usage_mode
2689 table: safehome_usage_mode
2690 - name: nav_mission_planner_reset
2691 description: "With Reset ON WP Mission Planner waypoint count can be reset to 0 by toggling the mode switch ON-OFF-ON."
2693 field: general.flags.mission_planner_reset
2695 - name: nav_cruise_yaw_rate
2696 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]"
2698 field: general.cruise_yaw_rate
2701 - name: nav_mc_bank_angle
2702 description: "Maximum banking angle (deg) that multicopter navigation is allowed to set. Machine must be able to satisfy this angle without loosing altitude"
2704 field: mc.max_bank_angle
2707 - name: nav_mc_auto_climb_rate
2708 description: "Maximum climb/descent rate that UAV is allowed to reach during navigation modes. [cm/s]"
2710 field: mc.max_auto_climb_rate
2713 - name: nav_mc_manual_climb_rate
2714 description: "Maximum climb/descent rate firmware is allowed when processing pilot input for ALTHOLD control mode [cm/s]"
2716 field: mc.max_manual_climb_rate
2719 - name: nav_auto_disarm_delay
2720 description: "Delay before craft disarms when `nav_disarm_on_landing` is set (ms)"
2722 field: general.auto_disarm_delay
2725 - name: nav_mc_braking_speed_threshold
2726 description: "min speed in cm/s above which braking can happen"
2728 field: mc.braking_speed_threshold
2729 condition: USE_MR_BRAKING_MODE
2732 - name: nav_mc_braking_disengage_speed
2733 description: "braking is disabled when speed goes below this value"
2735 field: mc.braking_disengage_speed
2736 condition: USE_MR_BRAKING_MODE
2739 - name: nav_mc_braking_timeout
2740 description: "timeout in ms for braking"
2742 field: mc.braking_timeout
2743 condition: USE_MR_BRAKING_MODE
2746 - name: nav_mc_braking_boost_factor
2747 description: "acceleration factor for BOOST phase"
2749 field: mc.braking_boost_factor
2750 condition: USE_MR_BRAKING_MODE
2753 - name: nav_mc_braking_boost_timeout
2754 description: "how long in ms BOOST phase can happen"
2756 field: mc.braking_boost_timeout
2757 condition: USE_MR_BRAKING_MODE
2760 - name: nav_mc_braking_boost_speed_threshold
2761 description: "BOOST can be enabled when speed is above this value"
2763 field: mc.braking_boost_speed_threshold
2764 condition: USE_MR_BRAKING_MODE
2767 - name: nav_mc_braking_boost_disengage_speed
2768 description: "BOOST will be disabled when speed goes below this value"
2770 field: mc.braking_boost_disengage_speed
2771 condition: USE_MR_BRAKING_MODE
2774 - name: nav_mc_braking_bank_angle
2775 description: "max angle that MR is allowed to bank in BOOST mode"
2777 field: mc.braking_bank_angle
2778 condition: USE_MR_BRAKING_MODE
2781 - name: nav_mc_pos_deceleration_time
2782 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"
2784 field: mc.posDecelerationTime
2787 - name: nav_mc_pos_expo
2788 description: "Expo for PosHold control"
2790 field: mc.posResponseExpo
2793 - name: nav_mc_wp_slowdown
2794 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."
2796 field: mc.slowDownForTurning
2798 - name: nav_fw_bank_angle
2799 description: "Max roll angle when rolling / turning in GPS assisted modes, is also restrained by global max_angle_inclination_rll"
2801 field: fw.max_bank_angle
2804 - name: nav_fw_manual_climb_rate
2805 description: "Maximum climb/descent rate firmware is allowed when processing pilot input for ALTHOLD control mode [cm/s]"
2807 field: fw.max_manual_climb_rate
2810 - name: nav_fw_climb_angle
2811 description: "Max pitch angle when climbing in GPS assisted modes, is also restrained by global max_angle_inclination_pit"
2813 field: fw.max_climb_angle
2816 - name: nav_fw_dive_angle
2817 description: "Max negative pitch angle when diving in GPS assisted modes, is also restrained by global max_angle_inclination_pit"
2819 field: fw.max_dive_angle
2822 - name: nav_fw_pitch2thr_smoothing
2823 description: "How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by pitch_to_throttle_thresh."
2825 field: fw.pitch_to_throttle_smooth
2828 - name: fw_min_throttle_down_pitch
2829 description: "Automatic pitch down angle when throttle is at 0 in angle mode. Progressively applied between cruise throttle and zero throttle (decidegrees)"
2831 field: fw.minThrottleDownPitchAngle
2834 - name: nav_fw_pitch2thr_threshold
2835 description: "Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees]"
2837 field: fw.pitch_to_throttle_thresh
2840 - name: nav_fw_loiter_radius
2841 description: "PosHold radius. 3000 to 7500 is a good value (30-75m) [cm]"
2843 field: fw.loiter_radius
2846 - name: fw_loiter_direction
2847 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."
2848 default_value: "RIGHT"
2849 field: fw.loiter_direction
2851 - name: nav_fw_cruise_speed
2852 description: "Speed for the plane/wing at cruise throttle used for remaining flight time/distance estimation in cm/s"
2854 field: fw.cruise_speed
2857 - name: nav_fw_control_smoothness
2858 description: "How smoothly the autopilot controls the airplane to correct the navigation error"
2860 field: fw.control_smoothness
2863 - name: nav_fw_land_dive_angle
2864 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"
2866 field: fw.land_dive_angle
2869 - name: nav_fw_launch_velocity
2870 description: "Forward velocity threshold for swing-launch detection [cm/s]"
2872 field: fw.launch_velocity_thresh
2875 - name: nav_fw_launch_accel
2876 description: "Forward acceleration threshold for bungee launch of throw launch [cm/s/s], 1G = 981 cm/s/s"
2878 field: fw.launch_accel_thresh
2881 - name: nav_fw_launch_max_angle
2882 description: "Max tilt angle (pitch/roll combined) to consider launch successful. Set to 180 to disable completely [deg]"
2884 field: fw.launch_max_angle
2887 - name: nav_fw_launch_detect_time
2888 description: "Time for which thresholds have to breached to consider launch happened [ms]"
2890 field: fw.launch_time_thresh
2893 - name: nav_fw_launch_idle_motor_delay
2894 description: "Delay between raising throttle and motor starting at idle throttle (ms)"
2896 field: fw.launch_idle_motor_timer
2899 - name: nav_fw_launch_motor_delay
2900 description: "Delay between detected launch and launch sequence start and throttling up (ms)"
2902 field: fw.launch_motor_timer
2905 - name: nav_fw_launch_spinup_time
2906 description: "Time to bring power from minimum throttle to nav_fw_launch_thr - to avoid big stress on ESC and large torque from propeller"
2908 field: fw.launch_motor_spinup_time
2911 - name: nav_fw_launch_end_time
2912 description: "Time for the transition of throttle and pitch angle, between the launch state and the subsequent flight mode [ms]"
2914 field: fw.launch_end_time
2917 - name: nav_fw_launch_min_time
2918 description: "Allow launch mode to execute at least this time (ms) and ignore stick movements [0-60000]."
2920 field: fw.launch_min_time
2923 - name: nav_fw_launch_timeout
2924 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)"
2926 field: fw.launch_timeout
2928 - name: nav_fw_launch_max_altitude
2929 description: "Altitude (centimeters) at which LAUNCH mode will be turned off and regular flight mode will take over [0-60000]."
2931 field: fw.launch_max_altitude
2934 - name: nav_fw_launch_climb_angle
2935 description: "Climb angle (attitude of model, not climb slope) for launch sequence (degrees), is also restrained by global max_angle_inclination_pit"
2937 field: fw.launch_climb_angle
2940 - name: nav_fw_launch_manual_throttle
2941 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)."
2943 field: fw.launch_manual_throttle
2945 - name: nav_fw_launch_land_abort_deadband
2946 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."
2948 field: fw.launch_land_abort_deadband
2951 - name: nav_fw_allow_manual_thr_increase
2952 description: "Enable the possibility to manually increase the throttle in auto throttle controlled modes for fixed wing"
2954 field: fw.allow_manual_thr_increase
2956 - name: nav_use_fw_yaw_control
2957 description: "Enables or Disables the use of the heading PID controller on fixed wing. Heading PID controller is always enabled for rovers and boats"
2959 field: fw.useFwNavYawControl
2961 - name: nav_fw_yaw_deadband
2962 description: "Deadband for heading trajectory PID controller. When heading error is below the deadband, controller assumes that vehicle is on course"
2964 field: fw.yawControlDeadband
2968 - name: PG_TELEMETRY_CONFIG
2969 type: telemetryConfig_t
2970 headers: ["io/serial.h", "telemetry/telemetry.h", "telemetry/sim.h"]
2971 condition: USE_TELEMETRY
2973 - name: telemetry_switch
2974 description: "Which aux channel to use to change serial output & baud rate (MSP / Telemetry). It disables automatic switching to Telemetry when armed."
2977 - name: telemetry_inverted
2978 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."
2981 - name: frsky_pitch_roll
2982 description: "S.Port telemetry: Send pitch and roll degrees*10 instead of raw accelerometer data"
2985 - name: report_cell_voltage
2986 description: "S.Port and IBUS telemetry: Send the average cell voltage if set to ON"
2989 - name: hott_alarm_sound_interval
2990 description: "Battery alarm delay in seconds for Hott telemetry"
2992 field: hottAlarmSoundInterval
2995 - name: telemetry_halfduplex
2996 description: "S.Port telemetry only: Turn UART into UNIDIR for usage on F1 and F4 target. See Telemetry.md for details"
3000 - name: smartport_fuel_unit
3001 description: "S.Port telemetry only: Unit of the value sent with the `FUEL` ID (FrSky D-Series always sends percent). [PERCENT/MAH/MWH]"
3002 default_value: "MAH"
3003 field: smartportFuelUnit
3004 condition: USE_TELEMETRY_SMARTPORT
3006 table: smartport_fuel_unit
3007 - name: ibus_telemetry_type
3008 description: "Type compatibility ibus telemetry for transmitters. See Telemetry.md label IBUS for details."
3010 field: ibusTelemetryType
3013 - name: ltm_update_rate
3014 description: "Defines the LTM update rate (use of bandwidth [NORMAL/MEDIUM/SLOW]). See Telemetry.md, LTM section for details."
3015 default_value: "NORMAL"
3016 field: ltmUpdateRate
3017 condition: USE_TELEMETRY_LTM
3019 - name: sim_ground_station_number
3020 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."
3022 field: simGroundStationNumber
3023 condition: USE_TELEMETRY_SIM
3025 description: "PIN code for the SIM module"
3026 default_value: "0000"
3028 condition: USE_TELEMETRY_SIM
3029 - name: sim_transmit_interval
3030 description: "Text message transmission interval in seconds for SIM module. Minimum value: 10"
3032 field: simTransmitInterval
3033 condition: USE_TELEMETRY_SIM
3035 min: SIM_MIN_TRANSMIT_INTERVAL
3037 - name: sim_transmit_flags
3038 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`"
3039 default_value: :SIM_TX_FLAG_FAILSAFE
3040 field: simTransmitFlags
3041 condition: USE_TELEMETRY_SIM
3043 - name: acc_event_threshold_high
3044 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."
3046 field: accEventThresholdHigh
3047 condition: USE_TELEMETRY_SIM
3051 - name: acc_event_threshold_low
3052 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."
3054 field: accEventThresholdLow
3055 condition: USE_TELEMETRY_SIM
3059 - name: acc_event_threshold_neg_x
3060 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."
3062 field: accEventThresholdNegX
3063 condition: USE_TELEMETRY_SIM
3067 - name: sim_low_altitude
3068 description: "Threshold for low altitude warning messages sent by SIM module when the 'L' transmit flag is set in `sim_transmit_flags`."
3069 default_value: -32767
3070 field: simLowAltitude
3071 condition: USE_TELEMETRY_SIM
3075 - name: mavlink_ext_status_rate
3076 field: mavlink.extended_status_rate
3081 - name: mavlink_rc_chan_rate
3082 field: mavlink.rc_channels_rate
3087 - name: mavlink_pos_rate
3088 field: mavlink.position_rate
3093 - name: mavlink_extra1_rate
3094 field: mavlink.extra1_rate
3099 - name: mavlink_extra2_rate
3100 field: mavlink.extra2_rate
3105 - name: mavlink_extra3_rate
3106 field: mavlink.extra3_rate
3111 - name: mavlink_version
3112 field: mavlink.version
3113 description: "Version of MAVLink to use"
3119 - name: PG_LED_STRIP_CONFIG
3120 type: ledStripConfig_t
3121 headers: ["common/color.h", "io/ledstrip.h"]
3122 condition: USE_LED_STRIP
3124 - name: ledstrip_visual_beeper
3129 - name: PG_OSD_CONFIG
3131 headers: ["io/osd.h", "drivers/osd.h"]
3134 - name: osd_telemetry
3135 description: "To enable OSD telemetry for antenna tracker. Possible values are `OFF`, `ON` and `TEST`"
3136 table: osd_telemetry
3139 default_value: "OFF"
3140 - name: osd_video_system
3141 description: "Video system used. Possible values are `AUTO`, `PAL`, `NTSC`, `HDZERO`, 'DJIWTF', 'AVATAR' and `BF43COMPAT`"
3142 default_value: "AUTO"
3143 table: osd_video_system
3146 - name: osd_row_shiftdown
3147 description: "Number of rows to shift the OSD display (increase if top rows are cut off)"
3149 field: row_shiftdown
3152 - name: osd_msp_displayport_fullframe_interval
3153 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)"
3158 field: msp_displayport_fullframe_interval
3160 description: "IMPERIAL, METRIC, UK"
3161 default_value: "METRIC"
3165 - name: osd_stats_energy_unit
3166 description: "Unit used for the drawn energy in the OSD stats [MAH/WH] (milliAmpere hour/ Watt hour)"
3167 default_value: "MAH"
3168 field: stats_energy_unit
3169 table: osd_stats_energy_unit
3171 - name: osd_stats_min_voltage_unit
3172 description: "Display minimum voltage of the `BATTERY` or the average per `CELL` in the OSD stats."
3173 default_value: "BATTERY"
3174 field: stats_min_voltage_unit
3175 table: osd_stats_min_voltage_unit
3177 - name: osd_stats_page_auto_swap_time
3178 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."
3180 field: stats_page_auto_swap_time
3183 - name: osd_rssi_alarm
3184 description: "Value below which to make the OSD RSSI indicator blink"
3189 - name: osd_time_alarm
3190 description: "Value above which to make the OSD flight time indicator blink (minutes)"
3195 - name: osd_alt_alarm
3196 description: "Value above which to make the OSD relative altitude indicator blink (meters)"
3201 - name: osd_dist_alarm
3202 description: "Value above which to make the OSD distance from home indicator blink (meters)"
3207 - name: osd_neg_alt_alarm
3208 description: "Value below which (negative altitude) to make the OSD relative altitude indicator blink (meters)"
3210 field: neg_alt_alarm
3213 - name: osd_current_alarm
3214 description: "Value above which the OSD current consumption element will start blinking. Measured in full Amperes."
3216 field: current_alarm
3219 - name: osd_gforce_alarm
3220 description: "Value above which the OSD g force indicator will blink (g)"
3225 - name: osd_gforce_axis_alarm_min
3226 description: "Value under which the OSD axis g force indicators will blink (g)"
3228 field: gforce_axis_alarm_min
3231 - name: osd_gforce_axis_alarm_max
3232 description: "Value above which the OSD axis g force indicators will blink (g)"
3234 field: gforce_axis_alarm_max
3237 - name: osd_imu_temp_alarm_min
3238 description: "Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3240 field: imu_temp_alarm_min
3243 - name: osd_imu_temp_alarm_max
3244 description: "Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3246 field: imu_temp_alarm_max
3249 - name: osd_esc_temp_alarm_max
3250 description: "Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3252 field: esc_temp_alarm_max
3255 - name: osd_esc_temp_alarm_min
3256 description: "Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade)"
3258 field: esc_temp_alarm_min
3261 - name: osd_baro_temp_alarm_min
3262 description: "Temperature under which the baro temperature OSD element will start blinking (decidegrees centigrade)"
3264 field: baro_temp_alarm_min
3268 - name: osd_baro_temp_alarm_max
3269 description: "Temperature above which the baro temperature OSD element will start blinking (decidegrees centigrade)"
3271 field: baro_temp_alarm_max
3275 - name: osd_snr_alarm
3276 condition: USE_SERIALRX_CRSF
3277 description: "Value below which Crossfire SNR Alarm pops-up. (dB)"
3282 - name: osd_link_quality_alarm
3283 condition: USE_SERIALRX_CRSF
3284 description: "LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%"
3286 field: link_quality_alarm
3289 - name: osd_rssi_dbm_alarm
3290 condition: USE_SERIALRX_CRSF
3291 description: "RSSI dBm indicator blinks below this value [dBm]. 0 disables this alarm"
3293 field: rssi_dbm_alarm
3296 - name: osd_rssi_dbm_max
3297 condition: USE_SERIALRX_CRSF
3298 description: "RSSI dBm upper end of curve. Perfect rssi (max) = 100%"
3303 - name: osd_rssi_dbm_min
3304 condition: USE_SERIALRX_CRSF
3305 description: "RSSI dBm lower end of curve or RX sensitivity level. Worst rssi (min) = 0%"
3310 - name: osd_temp_label_align
3311 description: "Allows to chose between left and right alignment for the OSD temperature sensor labels. Valid values are `LEFT` and `RIGHT`"
3312 default_value: "LEFT"
3313 field: temp_label_align
3314 condition: USE_TEMPERATURE_SENSOR
3315 table: osd_alignment
3317 - name: osd_airspeed_alarm_min
3318 condition: USE_PITOT
3319 description: "Airspeed under which the airspeed OSD element will start blinking (cm/s)"
3321 field: airspeed_alarm_min
3323 max: 27000 # (1000km/h * 1000 * 100 / 60 / 60)
3324 - name: osd_airspeed_alarm_max
3325 condition: USE_PITOT
3326 description: "Airspeed above which the airspeed OSD element will start blinking (cm/s)"
3328 field: airspeed_alarm_max
3330 max: 27000 # (1000km/h * 1000 * 100 / 60 / 60)
3331 - name: osd_ahi_reverse_roll
3332 description: "Switches the artificial horizon in the OSD to instead be a bank indicator, by reversing the direction of its movement."
3333 field: ahi_reverse_roll
3336 - name: osd_ahi_max_pitch
3337 description: "Max pitch, in degrees, for OSD artificial horizon"
3339 field: ahi_max_pitch
3343 - name: osd_crosshairs_style
3344 description: "To set the visual type for the crosshair"
3345 default_value: "DEFAULT"
3346 field: crosshairs_style
3347 table: osd_crosshairs_style
3349 - name: osd_crsf_lq_format
3350 description: "To select LQ format"
3351 default_value: "TYPE1"
3352 field: crsf_lq_format
3353 table: osd_crsf_lq_format
3355 - name: osd_horizon_offset
3356 description: "To vertically adjust the whole OSD and AHI and scrolling bars"
3358 field: horizon_offset
3361 - name: osd_camera_uptilt
3362 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)."
3364 field: camera_uptilt
3367 - name: osd_ahi_camera_uptilt_comp
3368 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)."
3370 field: ahi_camera_uptilt_comp
3372 - name: osd_camera_fov_h
3373 description: "Horizontal field of view for the camera in degres"
3378 - name: osd_camera_fov_v
3379 description: "Vertical field of view for the camera in degres"
3384 - name: osd_hud_margin_h
3385 description: "Left and right margins for the hud area"
3390 - name: osd_hud_margin_v
3391 description: "Top and bottom margins for the hud area"
3396 - name: osd_hud_homing
3397 description: "To display little arrows around the crossair showing where the home point is in the hud"
3401 - name: osd_hud_homepoint
3402 description: "To 3D-display the home point location in the hud"
3404 field: hud_homepoint
3406 - name: osd_hud_radar_disp
3407 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"
3409 field: hud_radar_disp
3412 - name: osd_hud_radar_range_min
3413 description: "In meters, radar aircrafts closer than this will not be displayed in the hud"
3415 field: hud_radar_range_min
3418 - name: osd_hud_radar_range_max
3419 description: "In meters, radar aircrafts further away than this will not be displayed in the hud"
3421 field: hud_radar_range_max
3424 - name: osd_hud_radar_alt_difference_display_time
3425 description: "Time in seconds to display the altitude difference in radar"
3426 field: hud_radar_alt_difference_display_time
3430 - name: osd_hud_radar_distance_display_time
3431 description: "Time in seconds to display the distance in radar"
3432 field: hud_radar_distance_display_time
3436 - name: osd_hud_wp_disp
3437 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)"
3442 - name: osd_left_sidebar_scroll
3443 field: left_sidebar_scroll
3444 table: osd_sidebar_scroll
3447 - name: osd_right_sidebar_scroll
3448 field: right_sidebar_scroll
3449 table: osd_sidebar_scroll
3452 - name: osd_sidebar_scroll_arrows
3453 field: sidebar_scroll_arrows
3456 - name: osd_main_voltage_decimals
3457 description: "Number of decimals for the battery voltages displayed in the OSD [1-2]."
3459 field: main_voltage_decimals
3462 - name: osd_coordinate_digits
3463 field: coordinate_digits
3468 - name: osd_adsb_distance_warning
3469 description: "Distance in meters of ADSB aircraft that is displayed"
3470 default_value: 20000
3472 field: adsb_distance_warning
3476 - name: osd_adsb_distance_alert
3477 description: "Distance inside which ADSB data flashes for proximity warning"
3480 field: adsb_distance_alert
3484 - name: osd_adsb_ignore_plane_above_me_limit
3485 description: "Ignore adsb planes above, limit, 0 disabled (meters)"
3488 field: adsb_ignore_plane_above_me_limit
3493 - name: osd_estimations_wind_compensation
3494 description: "Use wind estimation for remaining flight time/distance estimation"
3496 condition: USE_WIND_ESTIMATOR
3497 field: estimations_wind_compensation
3500 - name: osd_failsafe_switch_layout
3501 description: "If enabled the OSD automatically switches to the first layout during failsafe"
3505 - name: osd_plus_code_digits
3506 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."
3507 field: plus_code_digits
3511 - name: osd_plus_code_short
3512 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."
3513 field: plus_code_short
3515 table: osd_plus_code_short
3517 - name: osd_ahi_style
3518 description: "Sets OSD Artificial Horizon style \"DEFAULT\" or \"LINE\" for the FrSky Graphical OSD."
3520 default_value: "DEFAULT"
3521 table: osd_ahi_style
3524 - name: osd_force_grid
3528 description: Force OSD to work in grid mode even if the OSD device supports pixel level access (mainly used for development)
3530 - name: osd_ahi_bordered
3533 description: Shows a border/corners around the AHI region (pixel OSD only)
3536 - name: osd_ahi_width
3539 description: AHI width in pixels (pixel OSD only)
3542 - name: osd_ahi_height
3545 description: AHI height in pixels (pixel OSD only)
3548 - name: osd_ahi_vertical_offset
3549 field: ahi_vertical_offset
3552 description: AHI vertical offset from center (pixel OSD only)
3555 - name: osd_sidebar_horizontal_offset
3556 field: sidebar_horizontal_offset
3560 description: Sidebar horizontal offset from default position. Positive values move the sidebars closer to the edges.
3562 - name: osd_left_sidebar_scroll_step
3563 field: left_sidebar_scroll_step
3566 description: How many units each sidebar step represents. 0 means the default value for the scroll type.
3568 - name: osd_right_sidebar_scroll_step
3569 field: right_sidebar_scroll_step
3572 description: Same as left_sidebar_scroll_step, but for the right sidebar
3574 - name: osd_sidebar_height
3575 field: sidebar_height
3579 description: Height of sidebars in rows. 0 leaves only the level indicator arrows (Not for pixel OSD)
3581 - name: osd_ahi_pitch_interval
3582 field: ahi_pitch_interval
3586 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)
3588 - name: osd_home_position_arm_screen
3591 description: Should home position coordinates be displayed on the arming screen.
3593 - name: osd_pan_servo_index
3594 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.
3595 field: pan_servo_index
3600 - name: osd_pan_servo_pwm2centideg
3601 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.
3602 field: pan_servo_pwm2centideg
3607 - name: osd_pan_servo_offcentre_warning
3608 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.
3609 field: pan_servo_offcentre_warning
3614 - name: osd_pan_servo_indicator_show_degrees
3615 description: Show the degress of offset from centre on the pan servo OSD display element.
3616 field: pan_servo_indicator_show_degrees
3620 - name: osd_esc_rpm_precision
3621 description: Number of characters used to display the RPM value.
3622 field: esc_rpm_precision
3627 - name: osd_mah_precision
3628 description: Number of digits used for mAh precision. Currently used by mAh Used and Battery Remaining Capacity
3629 field: mAh_precision
3634 - name: osd_use_pilot_logo
3635 description: Use custom pilot logo with/instead of the INAV logo. The pilot logo must be characters 473 to 511
3636 field: use_pilot_logo
3640 - name: osd_inav_to_pilot_logo_spacing
3641 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.
3642 field: inav_to_pilot_logo_spacing
3647 - name: osd_arm_screen_display_time
3648 description: Amount of time to display the arm screen [ms]
3649 field: arm_screen_display_time
3654 - name: osd_switch_indicator_zero_name
3655 description: "Character to use for OSD switch incicator 0."
3656 field: osd_switch_indicator0_name
3659 default_value: "FLAP"
3661 - name: osd_switch_indicator_one_name
3662 description: "Character to use for OSD switch incicator 1."
3663 field: osd_switch_indicator1_name
3666 default_value: "GEAR"
3668 - name: osd_switch_indicator_two_name
3669 description: "Character to use for OSD switch incicator 2."
3670 field: osd_switch_indicator2_name
3673 default_value: "CAM"
3675 - name: osd_switch_indicator_three_name
3676 description: "Character to use for OSD switch incicator 3."
3677 field: osd_switch_indicator3_name
3680 default_value: "LIGT"
3682 - name: osd_switch_indicator_zero_channel
3683 description: "RC Channel to use for OSD switch indicator 0."
3684 field: osd_switch_indicator0_channel
3686 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3689 - name: osd_switch_indicator_one_channel
3690 description: "RC Channel to use for OSD switch indicator 1."
3691 field: osd_switch_indicator1_channel
3693 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3696 - name: osd_switch_indicator_two_channel
3697 description: "RC Channel to use for OSD switch indicator 2."
3698 field: osd_switch_indicator2_channel
3700 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3703 - name: osd_switch_indicator_three_channel
3704 description: "RC Channel to use for OSD switch indicator 3."
3705 field: osd_switch_indicator3_channel
3707 max: MAX_SUPPORTED_RC_CHANNEL_COUNT
3710 - name: osd_switch_indicators_align_left
3711 description: "Align text to left of switch indicators"
3712 field: osd_switch_indicators_align_left
3716 - name: osd_system_msg_display_time
3717 description: System message display cycle time for multiple messages (milliseconds).
3718 field: system_msg_display_time
3723 - name: PG_OSD_COMMON_CONFIG
3724 type: osdCommonConfig_t
3725 headers: ["io/osd_common.h"]
3726 condition: USE_OSD || USE_DJI_HD_OSD
3728 - name: osd_speed_source
3729 description: "Sets the speed type displayed by the DJI OSD and OSD canvas (FrSky Pixel): GROUND, 3D, AIR"
3730 default_value: "GROUND"
3732 table: osdSpeedSource
3735 - name: PG_SYSTEM_CONFIG
3736 type: systemConfig_t
3737 headers: ["fc/config.h"]
3740 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)"
3741 default_value: "400KHZ"
3744 - name: cpu_underclock
3745 description: "This option is only available on certain architectures (F3 CPUs at the moment). It makes CPU clock lower to reduce interference to long-range RC systems working at 433MHz"
3747 field: cpuUnderclock
3748 condition: USE_UNDERCLOCK
3751 description: "Defines debug values exposed in debug variables (developer / debugging setting)"
3752 default_value: "NONE"
3754 - name: ground_test_mode
3755 description: "For developer ground test use. Disables motors, sets heading status = Trusted on FW."
3756 condition: USE_DEV_TOOLS
3758 field: groundTestMode
3760 - name: throttle_tilt_comp_str
3761 description: "Can be used in ANGLE and HORIZON mode and will automatically boost throttle when banking. Setting is in percentage, 0=disabled."
3763 field: throttle_tilt_compensation_strength
3767 description: "Craft name"
3771 max: MAX_NAME_LENGTH
3773 description: "Pilot name"
3777 max: MAX_NAME_LENGTH
3779 - name: PG_MODE_ACTIVATION_OPERATOR_CONFIG
3780 type: modeActivationOperatorConfig_t
3781 headers: ["fc/rc_modes.h"]
3783 - name: mode_range_logic_operator
3784 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."
3786 field: modeActivationOperator
3790 - name: PG_STATS_CONFIG
3792 headers: ["fc/stats.h"]
3793 condition: USE_STATS
3796 description: "General switch of the statistics recording feature (a.k.a. odometer)"
3798 field: stats_enabled
3800 - name: stats_total_time
3801 description: "Total flight time [in seconds]. The value is updated on every disarm when \"stats\" are enabled."
3804 - name: stats_total_dist
3805 description: "Total flight distance [in meters]. The value is updated on every disarm when \"stats\" are enabled."
3808 - name: stats_total_energy
3809 description: "Total energy consumption [in mWh]. The value is updated on every disarm when \"stats\" are enabled."
3814 - name: PG_TIME_CONFIG
3816 headers: ["common/time.h"]
3819 description: "Time zone offset from UTC, in minutes. This is applied to the GPS time for logging and time-stamping of Blackbox logs"
3823 - name: tz_automatic_dst
3824 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`."
3825 default_value: "OFF"
3827 table: tz_automatic_dst
3829 - name: PG_DISPLAY_CONFIG
3830 type: displayConfig_t
3831 headers: ["drivers/display.h"]
3833 - name: display_force_sw_blink
3834 description: "OFF = OSD hardware blink / ON = OSD software blink. If OSD warning text/values are invisible, try setting this to ON"
3836 field: force_sw_blink
3839 - name: PG_VTX_CONFIG
3841 headers: ["io/vtx_control.h"]
3842 condition: USE_VTX_CONTROL
3844 - name: vtx_halfduplex
3845 description: "Use half duplex UART to communicate with the VTX, using only a TX pin in the FC."
3849 - name: vtx_smartaudio_early_akk_workaround
3850 description: "Enable workaround for early AKK SAudio-enabled VTX bug."
3852 field: smartAudioEarlyAkkWorkaroundEnable
3854 - name: vtx_smartaudio_alternate_softserial_method
3855 description: "Enable the alternate softserial method. This is the method used in INAV 3.0 and ealier."
3857 field: smartAudioAltSoftSerialMethod
3859 - name: vtx_softserial_shortstop
3860 description: "Enable the 3x shorter stopbit on softserial. Need for some IRC Tramp VTXes."
3862 field: softSerialShortStop
3864 - name: vtx_smartaudio_stopbits
3865 description: "Set stopbit count for serial (TBS Sixty9 SmartAudio 2.1 require value of 1 bit)"
3867 field: smartAudioStopBits
3871 - name: PG_VTX_SETTINGS_CONFIG
3872 type: vtxSettingsConfig_t
3873 headers: ["drivers/vtx_common.h", "io/vtx.h"]
3874 condition: USE_VTX_SMARTAUDIO || USE_VTX_TRAMP
3877 description: "Configure the VTX band. Bands: 1: A, 2: B, 3: E, 4: F, 5: Race."
3880 min: VTX_SETTINGS_MIN_BAND
3881 max: VTX_SETTINGS_MAX_BAND
3883 description: "Channel to use within the configured `vtx_band`. Valid values are [1, 8]."
3886 min: VTX_SETTINGS_MIN_CHANNEL
3887 max: VTX_SETTINGS_MAX_CHANNEL
3889 description: "VTX RF power level to use. The exact number of mw depends on the VTX hardware."
3892 min: VTX_SETTINGS_MIN_POWER
3893 max: VTX_SETTINGS_MAX_POWER
3894 - name: vtx_low_power_disarm
3895 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."
3896 default_value: "OFF"
3897 field: lowPowerDisarm
3898 table: vtx_low_power_disarm
3900 - name: vtx_pit_mode_chan
3902 min: VTX_SETTINGS_MIN_CHANNEL
3903 max: VTX_SETTINGS_MAX_CHANNEL
3905 - name: vtx_max_power_override
3906 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"
3908 field: maxPowerOverride
3911 - name: vtx_frequency_group
3912 field: frequencyGroup
3913 description: "VTx Frequency group to use. Frequency groups: FREQUENCYGROUP_5G8: 5.8GHz, FREQUENCYGROUP_2G4: 2.4GHz, FREQUENCYGROUP_1G3: 1.3GHz."
3914 table: vtx_frequency_groups
3917 default_value: FREQUENCYGROUP_5G8
3919 - name: PG_PINIOBOX_CONFIG
3920 type: pinioBoxConfig_t
3921 headers: ["io/piniobox.h"]
3922 condition: USE_PINIOBOX
3925 field: permanentId[0]
3926 description: "Mode assignment for PINIO#1"
3927 default_value: "target specific"
3930 default_value: :BOX_PERMANENT_ID_NONE
3933 field: permanentId[1]
3934 default_value: "target specific"
3935 description: "Mode assignment for PINIO#1"
3938 default_value: :BOX_PERMANENT_ID_NONE
3941 field: permanentId[2]
3942 default_value: "target specific"
3943 description: "Mode assignment for PINIO#1"
3946 default_value: :BOX_PERMANENT_ID_NONE
3949 field: permanentId[3]
3950 default_value: "target specific"
3951 description: "Mode assignment for PINIO#1"
3954 default_value: :BOX_PERMANENT_ID_NONE
3957 - name: PG_LOG_CONFIG
3959 headers: ["common/log.h"]
3965 description: "Defines serial debugging log level. See `docs/development/serial_printf_debugging.md` for usage."
3966 default_value: "ERROR"
3971 description: "Defines serial debugging log topic. See `docs/development/serial_printf_debugging.md` for usage."
3974 - name: PG_ESC_SENSOR_CONFIG
3975 type: escSensorConfig_t
3976 headers: ["sensors/esc_sensor.h"]
3977 condition: USE_ESC_SENSOR
3979 - name: esc_sensor_listen_only
3981 description: "Enable when BLHeli32 Auto Telemetry function is used. Disable in every other case"
3986 - name: PG_SMARTPORT_MASTER_CONFIG
3987 type: smartportMasterConfig_t
3988 headers: ["io/smartport_master.h"]
3989 condition: USE_SMARTPORT_MASTER
3991 - name: smartport_master_halfduplex
3995 - name: smartport_master_inverted
4000 - name: PG_DJI_OSD_CONFIG
4001 type: djiOsdConfig_t
4002 headers: ["io/osd_dji_hd.h"]
4003 condition: USE_DJI_HD_OSD
4005 - name: dji_workarounds
4006 description: "Enables workarounds for different versions of MSP protocol used"
4007 field: proto_workarounds
4011 - name: dji_use_name_for_messages
4012 description: "Re-purpose the craft name field for messages."
4014 field: use_name_for_messages
4016 - name: dji_esc_temp_source
4017 description: "Re-purpose the ESC temperature field for IMU/BARO temperature"
4018 default_value: "ESC"
4019 field: esc_temperature_source
4020 table: djiOsdTempSource
4022 - name: dji_message_speed_source
4023 description: "Sets the speed type displayed by the DJI OSD in craft name: GROUND, 3D, AIR"
4025 field: messageSpeedSource
4026 table: osdSpeedSource
4028 - name: dji_rssi_source
4029 description: "Source of the DJI RSSI field: RSSI, CRSF_LQ"
4030 default_value: "RSSI"
4032 table: djiRssiSource
4034 - name: dji_use_adjustments
4035 description: "Show inflight adjustments in craft name field"
4038 field: useAdjustments
4039 - name: dji_cn_alternating_duration
4040 description: "Alternating duration of craft name elements, in tenths of a second"
4044 field: craftNameAlternatingDuration
4047 - name: PG_BEEPER_CONFIG
4048 type: beeperConfig_t
4049 headers: [ "fc/config.h" ]
4051 - name: dshot_beeper_enabled
4052 description: "Whether using DShot motors as beepers is enabled"
4054 field: dshot_beeper_enabled
4056 - name: dshot_beeper_tone
4057 description: "Sets the DShot beeper tone"
4061 field: dshot_beeper_tone
4063 - name: beeper_pwm_mode
4067 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"
4069 - name: PG_POWER_LIMITS_CONFIG
4070 type: powerLimitsConfig_t
4071 headers: ["flight/power_limits.h"]
4072 condition: USE_POWER_LIMITS
4075 description: "Throttle attenuation PI control P term"
4080 description: "Throttle attenuation PI control I term"
4084 - name: limit_attn_filter_cutoff
4085 description: "Throttle attenuation PI control output filter cutoff frequency"
4087 field: attnFilterCutoff
4090 - name: PG_LEDPIN_CONFIG
4091 type: ledPinConfig_t
4092 headers: ["drivers/light_ws2811strip.h"]
4094 - name: led_pin_pwm_mode
4095 condition: USE_LED_STRIP
4096 description: "PWM mode of LED pin."
4097 default_value: "SHARED_LOW"
4098 field: led_pin_pwm_mode
4099 table: led_pin_pwm_mode
4101 - name: PG_OSD_JOYSTICK_CONFIG
4102 type: osdJoystickConfig_t
4103 headers: ["io/osd_joystick.h"]
4104 condition: USE_RCDEVICE && USE_LED_STRIP
4106 - name: osd_joystick_enabled
4107 description: "Enable OSD Joystick emulation"
4109 field: osd_joystick_enabled
4111 - name: osd_joystick_down
4112 description: "PWM value for DOWN key"
4114 field: osd_joystick_down
4117 - name: osd_joystick_up
4118 description: "PWM value for UP key"
4120 field: osd_joystick_up
4123 - name: osd_joystick_left
4124 description: "PWM value for LEFT key"
4126 field: osd_joystick_left
4129 - name: osd_joystick_right
4130 description: "PWM value for RIGHT key"
4132 field: osd_joystick_right
4135 - name: osd_joystick_enter
4136 description: "PWM value for ENTER key"
4138 field: osd_joystick_enter
4142 - name: PG_FW_AUTOLAND_CONFIG
4143 type: navFwAutolandConfig_t
4144 headers: ["navigation/navigation.h"]
4145 condition: USE_FW_AUTOLAND
4147 - name: nav_fw_land_approach_length
4148 description: "Length of the final approach"
4149 default_value: 35000
4150 field: approachLength
4153 - name: nav_fw_land_final_approach_pitch2throttle_mod
4154 description: "Modifier for pitch to throttle ratio at final approach. In Percent."
4156 field: finalApproachPitchToThrottleMod
4159 - name: nav_fw_land_glide_alt
4160 description: "Initial altitude of the glide phase"
4162 field: glideAltitude
4165 - name: nav_fw_land_flare_alt
4166 description: "Initial altitude of the flare phase"
4168 field: flareAltitude
4171 - name: nav_fw_land_glide_pitch
4172 description: "Pitch value for glide phase. In degrees."
4177 - name: nav_fw_land_flare_pitch
4178 description: "Pitch value for flare phase. In degrees"
4183 - name: nav_fw_land_max_tailwind
4184 description: "Max. tailwind (in cm/s) if no landing direction with downwind is available"