1 # CLI Variable Reference
3 > Note: this document is autogenerated. Do not edit it manually.
7 High value of throttle deadband for 3D mode (when stick is in the deadband range, the value in 3d_neutral is used instead)
9 | Default | Min | Max |
11 | 1514 | PWM_RANGE_MIN | PWM_RANGE_MAX |
17 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)
19 | Default | Min | Max |
21 | 1406 | PWM_RANGE_MIN | PWM_RANGE_MAX |
25 ### 3d_deadband_throttle
27 Throttle signal will be held to a fixed value when throttle is centered with an error margin defined in this parameter.
29 | Default | Min | Max |
37 Neutral (stop) throttle value for 3D mode
39 | Default | Min | Max |
41 | 1460 | PWM_RANGE_MIN | PWM_RANGE_MAX |
45 ### acc_event_threshold_high
47 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.
49 | Default | Min | Max |
55 ### acc_event_threshold_low
57 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.
59 | Default | Min | Max |
65 ### acc_event_threshold_neg_x
67 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.
69 | Default | Min | Max |
77 Selection of acc hardware. See Wiki Sensor auto detect and hardware failure detection for more info
79 | Default | Min | Max |
87 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.
89 | Default | Min | Max |
97 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.
99 | Default | Min | Max |
109 | Default | Min | Max |
119 | Default | Min | Max |
127 Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page.
129 | Default | Min | Max |
137 Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page.
139 | Default | Min | Max |
147 Calculated value after '6 position avanced calibration'. Uncalibrated value is 4096. See Wiki page.
149 | Default | Min | Max |
157 Calculated value after '6 position avanced calibration'. See Wiki page.
159 | Default | Min | Max |
161 | 0 | -32768 | 32767 |
167 Calculated value after '6 position avanced calibration'. See Wiki page.
169 | Default | Min | Max |
171 | 0 | -32768 | 32767 |
177 Calculated value after '6 position avanced calibration'. See Wiki page.
179 | Default | Min | Max |
181 | 0 | -32768 | 32767 |
185 ### airmode_throttle_threshold
187 Defines airmode THROTTLE activation threshold when `airmode_type` **THROTTLE_THRESHOLD** is used
189 | Default | Min | Max |
191 | 1150 | 1000 | 2000 |
197 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.
199 | Default | Min | Max |
205 ### airspeed_adc_channel
207 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
209 | Default | Min | Max |
211 | _target default_ | ADC_CHN_NONE | ADC_CHN_MAX |
215 ### align_board_pitch
217 Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc
219 | Default | Min | Max |
227 Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc
229 | Default | Min | Max |
237 Arbitrary board rotation in deci-degrees (0.1 degree), to allow mounting it sideways / upside down / rotated etc
239 | Default | Min | Max |
247 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.
249 | Default | Min | Max |
257 Same as align_mag_roll, but for the pitch axis.
259 | Default | Min | Max |
267 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.
269 | Default | Min | Max |
277 Same as align_mag_roll, but for the yaw axis.
279 | Default | Min | Max |
287 Optical flow module alignment (default CW0_DEG_FLIP)
289 | Default | Min | Max |
295 ### alt_hold_deadband
297 Defines the deadband of throttle during alt_hold [r/c points]
299 | Default | Min | Max |
305 ### antigravity_accelerator
309 | Default | Min | Max |
315 ### antigravity_cutoff_lpf_hz
317 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
319 | Default | Min | Max |
327 Max Antigravity gain. `1` means Antigravity is disabled, `2` means Iterm is allowed to double during rapid throttle movements
329 | Default | Min | Max |
337 Internal (configurator) hint. Should not be changed manually
339 | Default | Min | Max |
345 ### baro_cal_tolerance
347 Baro calibration tolerance in cm. The default should allow the noisiest baro to complete calibration [cm].
349 | Default | Min | Max |
357 Selection of baro hardware. See Wiki Sensor auto detect and hardware failure detection for more info
359 | Default | Min | Max |
367 Number of cells of the battery (0 = auto-detect), see battery documentation. 7S, 9S and 11S batteries cannot be auto-detected.
369 | Default | Min | Max |
377 Chose between raw and sag compensated battery voltage to use for battery alarms and telemetry. Possible values are `RAW` and `SAG_COMP`
379 | Default | Min | Max |
387 Set the battery capacity in mAh or mWh (see `battery_capacity_unit`). Used to calculate the remaining battery capacity.
389 | Default | Min | Max |
391 | 0 | 0 | 4294967295 |
395 ### battery_capacity_critical
397 If the remaining battery capacity goes below this threshold the battery is considered empty and the beeper will emit long beeps.
399 | Default | Min | Max |
401 | 0 | 0 | 4294967295 |
405 ### battery_capacity_unit
407 Unit used for `battery_capacity`, `battery_capacity_warning` and `battery_capacity_critical` [MAH/MWH] (milliAmpere hour / milliWatt hour).
409 | Default | Min | Max |
415 ### battery_capacity_warning
417 If the remaining battery capacity goes below this threshold the beeper will emit short beeps and the relevant OSD items will blink.
419 | Default | Min | Max |
421 | 0 | 0 | 4294967295 |
427 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
429 | Default | Min | Max |
437 Selection of where to write blackbox data
439 | Default | Min | Max |
441 | _target default_ | | |
445 ### blackbox_rate_denom
447 Blackbox logging rate denominator. See blackbox_rate_num.
449 | Default | Min | Max |
455 ### blackbox_rate_num
457 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
459 | Default | Min | Max |
467 Stick deadband in [r/c points], applied after r/c deadband and expo. Used to check if sticks are centered.
469 | Default | Min | Max |
475 ### controlrate_profile
477 Control rate profile to switch to when the battery profile is selected, 0 to disable and keep the currently selected control rate profile
479 | Default | Min | Max |
487 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
489 | Default | Min | Max |
497 Power draw at cruise throttle used for remaining flight time/distance estimation in 0.01W unit
499 | Default | Min | Max |
501 | 0 | 0 | 4294967295 |
505 ### current_adc_channel
507 ADC channel to use for analog current sensor input. Defaults to board CURRENT sensor input (if available). 0 = disabled
509 | Default | Min | Max |
511 | _target default_ | ADC_CHN_NONE | ADC_CHN_MAX |
515 ### current_meter_offset
517 This sets the output offset voltage of the current sensor in millivolts.
519 | Default | Min | Max |
521 | _target default_ | -32768 | 32767 |
525 ### current_meter_scale
527 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.
529 | Default | Min | Max |
531 | _target default_ | -10000 | 10000 |
535 ### current_meter_type
537 ADC , VIRTUAL, NONE. The virtual current sensor, once calibrated, estimates the current value from throttle position.
539 | Default | Min | Max |
545 ### d_boost_gyro_delta_lpf_hz
549 | Default | Min | Max |
559 | Default | Min | Max |
565 ### d_boost_max_at_acceleration
569 | Default | Min | Max |
571 | 7500 | 1000 | 16000 |
579 | Default | Min | Max |
587 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.
589 | Default | Min | Max |
597 Defines debug values exposed in debug variables (developer / debugging setting)
599 | Default | Min | Max |
605 ### disarm_kill_switch
607 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.
609 | Default | Min | Max |
615 ### display_force_sw_blink
617 OFF = OSD hardware blink / ON = OSD software blink. If OSD warning text/values are invisible, try setting this to ON
619 | Default | Min | Max |
625 ### dji_cn_alternating_duration
627 Alternating duration of craft name elements, in tenths of a second
629 | Default | Min | Max |
635 ### dji_esc_temp_source
637 Re-purpose the ESC temperature field for IMU/BARO temperature
639 | Default | Min | Max |
645 ### dji_message_speed_source
647 Sets the speed type displayed by the DJI OSD in craft name: GROUND, 3D, AIR
649 | Default | Min | Max |
657 Source of the DJI RSSI field: RSSI, CRSF_LQ
659 | Default | Min | Max |
665 ### dji_use_adjustments
667 Show inflight adjustments in craft name field
669 | Default | Min | Max |
675 ### dji_use_name_for_messages
677 Re-purpose the craft name field for messages.
679 | Default | Min | Max |
687 Enables workarounds for different versions of MSP protocol used
689 | Default | Min | Max |
695 ### dshot_beeper_enabled
697 Whether using DShot motors as beepers is enabled
699 | Default | Min | Max |
705 ### dshot_beeper_tone
707 Sets the DShot beeper tone
709 | Default | Min | Max |
717 Cutoff frequency for stage 2 D-term low pass filter
719 | Default | Min | Max |
727 Defines the type of stage 1 D-term LPF filter. Possible values: `PT1`, `BIQUAD`, `PT2`, `PT3`.
729 | Default | Min | Max |
737 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
739 | Default | Min | Max |
747 Defines the type of stage 1 D-term LPF filter. Possible values: `PT1`, `BIQUAD`, `PT2`, `PT3`.
749 | Default | Min | Max |
755 ### dynamic_gyro_notch_3d_q
757 Q factor for 3D dynamic notches
759 | Default | Min | Max |
765 ### dynamic_gyro_notch_enabled
767 Enable/disable dynamic gyro notch also known as Matrix Filter
769 | Default | Min | Max |
775 ### dynamic_gyro_notch_min_hz
777 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`
779 | Default | Min | Max |
785 ### dynamic_gyro_notch_mode
787 Gyro dynamic notch type
789 | Default | Min | Max |
795 ### dynamic_gyro_notch_q
797 Q factor for dynamic notches
799 | Default | Min | Max |
805 ### esc_sensor_listen_only
807 Enable when BLHeli32 Auto Telemetry function is used. Disable in every other case
809 | Default | Min | Max |
817 Time in deciseconds to wait before activating failsafe when signal is lost. See [Failsafe documentation](Failsafe.md#failsafe_delay).
819 | Default | Min | Max |
825 ### failsafe_fw_pitch_angle
827 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
829 | Default | Min | Max |
835 ### failsafe_fw_roll_angle
837 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
839 | Default | Min | Max |
841 | -200 | -800 | 800 |
845 ### failsafe_fw_yaw_rate
847 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
849 | Default | Min | Max |
851 | -45 | -1000 | 1000 |
857 Enable or disable the lights when the `FAILSAFE` flight mode is enabled. The target needs to be compiled with `USE_LIGHTS` [ON/OFF].
859 | Default | Min | Max |
865 ### failsafe_lights_flash_on_time
867 Flash lights ON time in milliseconds when `failsafe_lights` is ON and `FAILSAFE` flight mode is enabled. [20-65535].
869 | Default | Min | Max |
875 ### failsafe_lights_flash_period
877 Time in milliseconds between two flashes when `failsafe_lights` is ON and `FAILSAFE` flight mode is enabled [40-65535].
879 | Default | Min | Max |
881 | 1000 | 40 | 65535 |
885 ### failsafe_min_distance
887 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.
889 | Default | Min | Max |
895 ### failsafe_min_distance_procedure
897 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).
899 | Default | Min | Max |
905 ### failsafe_mission_delay
907 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.
909 | Default | Min | Max |
915 ### failsafe_off_delay
917 Time in deciseconds to wait before turning off motors when failsafe is activated. 0 = No timeout. See [Failsafe documentation](Failsafe.md#failsafe_off_delay).
919 | Default | Min | Max |
925 ### failsafe_procedure
927 What failsafe procedure to initiate in Stage 2. See [Failsafe documentation](Failsafe.md#failsafe_throttle).
929 | Default | Min | Max |
935 ### failsafe_recovery_delay
937 Time in deciseconds to wait before aborting failsafe when signal is recovered. See [Failsafe documentation](Failsafe.md#failsafe_recovery_delay).
939 | Default | Min | Max |
945 ### failsafe_stick_threshold
947 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.
949 | Default | Min | Max |
955 ### failsafe_throttle
957 Throttle level used for landing when failsafe is enabled. See [Failsafe documentation](Failsafe.md#failsafe_throttle).
959 | Default | Min | Max |
961 | 1000 | PWM_RANGE_MIN | PWM_RANGE_MAX |
965 ### failsafe_throttle_low_delay
967 If failsafe activated when throttle is low for this much time - bypass failsafe and disarm, in 10th of seconds. 0 = No timeout
969 | Default | Min | Max |
975 ### fixed_wing_auto_arm
977 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.
979 | Default | Min | Max |
985 ### flaperon_throw_offset
987 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.
989 | Default | Min | Max |
991 | 200 | FLAPERON_THROW_MIN | FLAPERON_THROW_MAX |
999 | Default | Min | Max |
1005 ### frsky_coordinates_format
1007 D-Series telemetry only: FRSKY_FORMAT_DMS (default), FRSKY_FORMAT_NMEA
1009 | Default | Min | Max |
1011 | 0 | 0 | FRSKY_FORMAT_NMEA |
1015 ### frsky_default_latitude
1017 D-Series telemetry only: OpenTX needs a valid set of coordinates to show compass value. A fake value defined in this setting is sent while no fix is acquired.
1019 | Default | Min | Max |
1025 ### frsky_default_longitude
1027 D-Series telemetry only: OpenTX needs a valid set of coordinates to show compass value. A fake value defined in this setting is sent while no fix is acquired.
1029 | Default | Min | Max |
1035 ### frsky_pitch_roll
1037 S.Port and D-Series telemetry: Send pitch and roll degrees*10 instead of raw accelerometer data
1039 | Default | Min | Max |
1047 Not used? [METRIC/IMPERIAL]
1049 | Default | Min | Max |
1055 ### frsky_vfas_precision
1057 D-Series telemetry only: Set to 1 to send raw VBat value in 0.1V resolution for receivers that can handle it, or 0 (default) to use the standard method
1059 | Default | Min | Max |
1061 | 0 | FRSKY_VFAS_PRECISION_LOW | FRSKY_VFAS_PRECISION_HIGH |
1065 ### fw_autotune_max_rate_deflection
1067 The target percentage of maximum mixer output used for determining the rates in `AUTO` and `LIMIT`.
1069 | Default | Min | Max |
1075 ### fw_autotune_min_stick
1077 Minimum stick input [%], after applying deadband and expo, to start recording the plane's response to stick input.
1079 | Default | Min | Max |
1085 ### fw_autotune_rate_adjustment
1087 `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.
1089 | Default | Min | Max |
1097 Fixed-wing attitude stabilisation HORIZON transition point
1099 | Default | Min | Max |
1107 Fixed wing rate stabilisation D-gain for PITCH
1109 | Default | Min | Max |
1117 Fixed wing rate stabilisation D-gain for ROLL
1119 | Default | Min | Max |
1127 Fixed wing rate stabilisation D-gain for YAW
1129 | Default | Min | Max |
1137 Fixed-wing rate stabilisation FF-gain for PITCH
1139 | Default | Min | Max |
1147 Fixed-wing rate stabilisation FF-gain for ROLL
1149 | Default | Min | Max |
1157 Fixed-wing rate stabilisation FF-gain for YAW
1159 | Default | Min | Max |
1167 Fixed-wing attitude stabilisation low-pass filter cutoff
1169 | Default | Min | Max |
1177 Fixed-wing rate stabilisation I-gain for PITCH
1179 | Default | Min | Max |
1187 Fixed-wing rate stabilisation I-gain for ROLL
1189 | Default | Min | Max |
1197 Fixed-wing rate stabilisation I-gain for YAW
1199 | Default | Min | Max |
1205 ### fw_iterm_limit_stick_position
1207 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
1209 | Default | Min | Max |
1215 ### fw_iterm_throw_limit
1217 Limits max/min I-term value in stabilization PID controller in case of Fixed Wing. It solves the problem of servo saturation before take-off/throwing the airplane into the air. By default, error accumulated in I-term can not exceed 1/3 of servo throw (around 165us). Set 0 to disable completely.
1219 | Default | Min | Max |
1221 | 165 | FW_ITERM_THROW_LIMIT_MIN | FW_ITERM_THROW_LIMIT_MAX |
1225 ### fw_level_pitch_gain
1227 I-gain for the pitch trim for self-leveling flight modes. Higher values means that AUTOTRIM will be faster but might introduce oscillations
1229 | Default | Min | Max |
1235 ### fw_level_pitch_trim
1237 Pitch trim for self-leveling flight modes. In degrees. +5 means airplane nose should be raised 5 deg from level
1239 | Default | Min | Max |
1245 ### fw_loiter_direction
1247 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.
1249 | Default | Min | Max |
1255 ### fw_min_throttle_down_pitch
1257 Automatic pitch down angle when throttle is at 0 in angle mode. Progressively applied between cruise throttle and zero throttle (decidegrees)
1259 | Default | Min | Max |
1267 Fixed-wing attitude stabilisation P-gain
1269 | Default | Min | Max |
1277 Fixed-wing rate stabilisation P-gain for PITCH
1279 | Default | Min | Max |
1287 Fixed-wing rate stabilisation P-gain for ROLL
1289 | Default | Min | Max |
1297 Fixed-wing rate stabilisation P-gain for YAW
1299 | Default | Min | Max |
1305 ### fw_reference_airspeed
1307 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.
1309 | Default | Min | Max |
1311 | 1500 | 300 | 6000 |
1315 ### fw_tpa_time_constant
1317 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.
1319 | Default | Min | Max |
1325 ### fw_turn_assist_pitch_gain
1327 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
1329 | Default | Min | Max |
1335 ### fw_turn_assist_yaw_gain
1337 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
1339 | Default | Min | Max |
1345 ### fw_yaw_iterm_freeze_bank_angle
1347 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.
1349 | Default | Min | Max |
1357 Automatic configuration of GPS baudrate(The specified baudrate in configured in ports will be used) when used with UBLOX GPS
1359 | Default | Min | Max |
1367 Enable automatic configuration of UBlox GPS receivers.
1369 | Default | Min | Max |
1377 GPS navigation model: Pedestrian, Air_1g, Air_4g. Default is AIR_1G. Use pedestrian with caution, can cause flyaways with fast flying.
1379 | Default | Min | Max |
1387 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.
1389 | Default | Min | Max |
1397 Which GPS protocol to be used, note that UBLOX is 5Hz and UBLOX7 is 10Hz (M8N).
1399 | Default | Min | Max |
1407 Which SBAS mode to be used
1409 | Default | Min | Max |
1415 ### gps_ublox_use_galileo
1417 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].
1419 | Default | Min | Max |
1425 ### ground_test_mode
1427 For developer ground test use. Disables motors, sets heading status = Trusted on FW.
1429 | Default | Min | Max |
1435 ### gyro_anti_aliasing_lpf_hz
1437 Gyro processing anti-aliasing filter cutoff frequency. In normal operation this filter setting should never be changed. In Hz
1439 | Default | Min | Max |
1445 ### gyro_anti_aliasing_lpf_type
1447 Specifies the type of the software LPF of the gyro signals.
1449 | Default | Min | Max |
1455 ### gyro_dyn_lpf_curve_expo
1457 Expo value for the throttle-to-frequency mapping for Dynamic LPF
1459 | Default | Min | Max |
1465 ### gyro_dyn_lpf_max_hz
1467 Maximum frequency of the gyro Dynamic LPF
1469 | Default | Min | Max |
1475 ### gyro_dyn_lpf_min_hz
1477 Minimum frequency of the gyro Dynamic LPF
1479 | Default | Min | Max |
1485 ### gyro_hardware_lpf
1487 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.
1489 | Default | Min | Max |
1495 ### gyro_main_lpf_hz
1497 Software based gyro main lowpass filter. Value is cutoff frequency (Hz)
1499 | Default | Min | Max |
1505 ### gyro_main_lpf_type
1507 Defines the type of the main gyro LPF filter. Possible values: `PT1`, `BIQUAD`. `PT1` offers faster filter response while `BIQUAD` better attenuation.
1509 | Default | Min | Max |
1519 | Default | Min | Max |
1525 ### gyro_use_dyn_lpf
1527 Use Dynamic LPF instead of static gyro stage1 LPF. Dynamic Gyro LPF updates gyro LPF based on the throttle position.
1529 | Default | Min | Max |
1537 Calculated gyro zero calibration of axis X
1539 | Default | Min | Max |
1541 | 0 | -32768 | 32767 |
1547 Calculated gyro zero calibration of axis Y
1549 | Default | Min | Max |
1551 | 0 | -32768 | 32767 |
1557 Calculated gyro zero calibration of axis Z
1559 | Default | Min | Max |
1561 | 0 | -32768 | 32767 |
1567 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
1569 | Default | Min | Max |
1575 ### heading_hold_rate_limit
1577 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.
1579 | Default | Min | Max |
1581 | 90 | HEADING_HOLD_RATE_LIMIT_MIN | HEADING_HOLD_RATE_LIMIT_MAX |
1585 ### hott_alarm_sound_interval
1587 Battery alarm delay in seconds for Hott telemetry
1589 | Default | Min | Max |
1597 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)
1599 | Default | Min | Max |
1605 ### ibus_telemetry_type
1607 Type compatibility ibus telemetry for transmitters. See Telemetry.md label IBUS for details.
1609 | Default | Min | Max |
1617 Power draw at zero throttle used for remaining flight time/distance estimation in 0.01W unit
1619 | Default | Min | Max |
1625 ### imu_acc_ignore_rate
1627 Total gyro rotation rate threshold [deg/s] before scaling to consider accelerometer trustworthy
1629 | Default | Min | Max |
1635 ### imu_acc_ignore_slope
1637 Half-width of the interval to gradually reduce accelerometer weight. Centered at `imu_acc_ignore_rate` (exactly 50% weight)
1639 | Default | Min | Max |
1647 Inertial Measurement Unit KI Gain for accelerometer measurements
1649 | Default | Min | Max |
1657 Inertial Measurement Unit KI Gain for compass measurements
1659 | Default | Min | Max |
1667 Inertial Measurement Unit KP Gain for accelerometer measurements
1669 | Default | Min | Max |
1677 Inertial Measurement Unit KP Gain for compass measurements
1679 | Default | Min | Max |
1685 ### imu_gps_yaw_windcomp
1687 Wind compensation in heading estimation from gps groundcourse(fixed wing only)
1689 | Default | Min | Max |
1695 ### imu_inertia_comp_method
1697 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
1699 | Default | Min | Max |
1705 ### inav_allow_dead_reckoning
1707 Defines if INAV will dead-reckon over short GPS outages. May also be useful for indoors OPFLOW navigation
1709 | Default | Min | Max |
1715 ### inav_auto_mag_decl
1717 Automatic setting of magnetic declination based on GPS position. When used manual magnetic declination is ignored.
1719 | Default | Min | Max |
1727 Uncertainty value for barometric sensor [cm]
1729 | Default | Min | Max |
1735 ### inav_gravity_cal_tolerance
1737 Unarmed gravity calibration tolerance level. Won't finish the calibration until estimated gravity error falls below this value.
1739 | Default | Min | Max |
1745 ### inav_max_eph_epv
1747 Maximum uncertainty value until estimated position is considered valid and is used for navigation [cm]
1749 | Default | Min | Max |
1755 ### inav_max_surface_altitude
1757 Max allowed altitude for surface following mode. [cm]
1759 | Default | Min | Max |
1765 ### inav_reset_altitude
1767 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)
1769 | Default | Min | Max |
1777 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
1779 | Default | Min | Max |
1785 ### inav_use_gps_no_baro
1789 | Default | Min | Max |
1795 ### inav_use_gps_velned
1797 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.
1799 | Default | Min | Max |
1807 Weight for accelerometer drift estimation
1809 | Default | Min | Max |
1815 ### inav_w_xy_flow_p
1819 | Default | Min | Max |
1825 ### inav_w_xy_flow_v
1829 | Default | Min | Max |
1837 Weight of GPS coordinates in estimated UAV position and speed.
1839 | Default | Min | Max |
1847 Weight of GPS velocity data in estimated UAV speed
1849 | Default | Min | Max |
1857 Decay coefficient for estimated velocity when GPS reference for position is lost
1859 | Default | Min | Max |
1865 ### inav_w_xyz_acc_p
1869 | Default | Min | Max |
1877 Weight of barometer measurements in estimated altitude and climb rate
1879 | Default | Min | Max |
1887 Weight of GPS altitude measurements in estimated altitude. Setting is used only of airplanes
1889 | Default | Min | Max |
1897 Weight of GPS climb rate measurements in estimated climb rate. Setting is used on both airplanes and multirotors. If GPS doesn't support native climb rate reporting (i.e. NMEA GPS) you may consider setting this to zero
1899 | Default | Min | Max |
1907 Decay coefficient for estimated climb rate when baro/GPS reference for altitude is lost
1909 | Default | Min | Max |
1915 ### inav_w_z_surface_p
1919 | Default | Min | Max |
1925 ### inav_w_z_surface_v
1929 | Default | Min | Max |
1937 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.
1939 | Default | Min | Max |
1945 ### ins_gravity_cmss
1947 Calculated 1G of Acc axis Z to use in INS
1949 | Default | Min | Max |
1957 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)
1959 | Default | Min | Max |
1965 ### ledstrip_visual_beeper
1969 | Default | Min | Max |
1975 ### limit_attn_filter_cutoff
1977 Throttle attenuation PI control output filter cutoff frequency
1979 | Default | Min | Max |
1985 ### limit_burst_current
1987 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
1989 | Default | Min | Max |
1995 ### limit_burst_current_falldown_time
1997 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`
1999 | Default | Min | Max |
2005 ### limit_burst_current_time
2007 Allowed current burst time (ds) during which `limit_burst_current` is allowed and after which `limit_cont_current` will be enforced
2009 | Default | Min | Max |
2015 ### limit_burst_power
2017 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
2019 | Default | Min | Max |
2025 ### limit_burst_power_falldown_time
2027 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`
2029 | Default | Min | Max |
2035 ### limit_burst_power_time
2037 Allowed power burst time (ds) during which `limit_burst_power` is allowed and after which `limit_cont_power` will be enforced
2039 | Default | Min | Max |
2045 ### limit_cont_current
2047 Continous current limit (dA), set to 0 to disable
2049 | Default | Min | Max |
2055 ### limit_cont_power
2057 Continous power limit (dW), set to 0 to disable
2059 | Default | Min | Max |
2067 Throttle attenuation PI control I term
2069 | Default | Min | Max |
2077 Throttle attenuation PI control P term
2079 | Default | Min | Max |
2087 Defines serial debugging log level. See `docs/development/serial_printf_debugging.md` for usage.
2089 | Default | Min | Max |
2097 Defines serial debugging log topic. See `docs/development/serial_printf_debugging.md` for usage.
2099 | Default | Min | Max |
2101 | 0 | 0 | 4294967295 |
2107 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.
2109 | Default | Min | Max |
2117 Defines the LTM update rate (use of bandwidth [NORMAL/MEDIUM/SLOW]). See Telemetry.md, LTM section for details.
2119 | Default | Min | Max |
2125 ### mag_calibration_time
2127 Adjust how long time the Calibration of mag will last.
2129 | Default | Min | Max |
2137 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.
2139 | Default | Min | Max |
2141 | 0 | -18000 | 18000 |
2147 Selection of mag hardware. See Wiki Sensor auto detect and hardware failure detection for more info
2149 | Default | Min | Max |
2157 Allow to chose between built-in and external compass sensor if they are connected to separate buses. Currently only for REVO target
2159 | Default | Min | Max |
2167 Magnetometer calibration X gain. If 1024, no calibration or calibration failed
2169 | Default | Min | Max |
2171 | 1024 | -32768 | 32767 |
2177 Magnetometer calibration Y gain. If 1024, no calibration or calibration failed
2179 | Default | Min | Max |
2181 | 1024 | -32768 | 32767 |
2187 Magnetometer calibration Z gain. If 1024, no calibration or calibration failed
2189 | Default | Min | Max |
2191 | 1024 | -32768 | 32767 |
2197 Magnetometer calibration X offset. If its 0 none offset has been applied and calibration is failed.
2199 | Default | Min | Max |
2201 | 0 | -32768 | 32767 |
2207 Magnetometer calibration Y offset. If its 0 none offset has been applied and calibration is failed.
2209 | Default | Min | Max |
2211 | 0 | -32768 | 32767 |
2217 Magnetometer calibration Z offset. If its 0 none offset has been applied and calibration is failed.
2219 | Default | Min | Max |
2221 | 0 | -32768 | 32767 |
2225 ### manual_pitch_rate
2227 Servo travel multiplier for the PITCH axis in `MANUAL` flight mode [0-100]%
2229 | Default | Min | Max |
2237 Exposition value used for the PITCH/ROLL axes by the `MANUAL` flight mode [0-100]
2239 | Default | Min | Max |
2245 ### manual_rc_yaw_expo
2247 Exposition value used for the YAW axis by the `MANUAL` flight mode [0-100]
2249 | Default | Min | Max |
2255 ### manual_roll_rate
2257 Servo travel multiplier for the ROLL axis in `MANUAL` flight mode [0-100]%
2259 | Default | Min | Max |
2267 Servo travel multiplier for the YAW axis in `MANUAL` flight mode [0-100]%
2269 | Default | Min | Max |
2275 ### mavlink_ext_status_rate
2279 | Default | Min | Max |
2285 ### mavlink_extra1_rate
2289 | Default | Min | Max |
2295 ### mavlink_extra2_rate
2299 | Default | Min | Max |
2305 ### mavlink_extra3_rate
2309 | Default | Min | Max |
2315 ### mavlink_pos_rate
2319 | Default | Min | Max |
2325 ### mavlink_rc_chan_rate
2329 | Default | Min | Max |
2337 Version of MAVLink to use
2339 | Default | Min | Max |
2345 ### max_angle_inclination_pit
2347 Maximum inclination in level (angle) mode (PITCH axis). 100=10°
2349 | Default | Min | Max |
2355 ### max_angle_inclination_rll
2357 Maximum inclination in level (angle) mode (ROLL axis). 100=10°
2359 | Default | Min | Max |
2367 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.
2369 | Default | Min | Max |
2371 | 1900 | PWM_RANGE_MIN | PWM_RANGE_MAX |
2377 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.
2379 | Default | Min | Max |
2381 | 1850 | PWM_RANGE_MIN | PWM_RANGE_MAX |
2387 Cutoff frequency for Control Derivative. Lower value smoother reaction on fast stick movements. With higher values, response will be more aggressive, jerky
2389 | Default | Min | Max |
2397 Multicopter Control Derivative gain for PITCH
2399 | Default | Min | Max |
2407 Multicopter Control Derivative gain for ROLL
2409 | Default | Min | Max |
2417 Multicopter Control Derivative gain for YAW
2419 | Default | Min | Max |
2427 Multicopter attitude stabilisation HORIZON transition point
2429 | Default | Min | Max |
2437 Multicopter rate stabilisation D-gain for PITCH
2439 | Default | Min | Max |
2447 Multicopter rate stabilisation D-gain for ROLL
2449 | Default | Min | Max |
2457 Multicopter rate stabilisation D-gain for YAW
2459 | Default | Min | Max |
2467 Multicopter attitude stabilisation low-pass filter cutoff
2469 | Default | Min | Max |
2477 Multicopter rate stabilisation I-gain for PITCH
2479 | Default | Min | Max |
2487 Multicopter rate stabilisation I-gain for ROLL
2489 | Default | Min | Max |
2497 Multicopter rate stabilisation I-gain for YAW
2499 | Default | Min | Max |
2509 | Default | Min | Max |
2515 ### mc_iterm_relax_cutoff
2519 | Default | Min | Max |
2527 Multicopter attitude stabilisation P-gain
2529 | Default | Min | Max |
2537 Multicopter rate stabilisation P-gain for PITCH
2539 | Default | Min | Max |
2547 Multicopter rate stabilisation P-gain for ROLL
2549 | Default | Min | Max |
2557 Multicopter rate stabilisation P-gain for YAW
2559 | Default | Min | Max |
2567 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.
2569 | Default | Min | Max |
2571 | 1100 | PWM_RANGE_MIN | PWM_RANGE_MAX |
2577 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.
2579 | Default | Min | Max |
2581 | 1000 | 0 | PWM_RANGE_MAX |
2585 ### mode_range_logic_operator
2587 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.
2589 | Default | Min | Max |
2595 ### model_preview_type
2597 ID of mixer preset applied in a Configurator. **Do not modify manually**. Used only for backup/restore reasons.
2599 | Default | Min | Max |
2607 When powering up, gyro bias is calculated. If the model is shaking/moving during this initial calibration, offsets are calculated incorrectly, and could lead to poor flying performance. This threshold means how much average gyro reading could differ before re-calibration is triggered.
2609 | Default | Min | Max |
2615 ### motor_direction_inverted
2617 Use if you need to inverse yaw motor direction.
2619 | Default | Min | Max |
2627 The number of motor poles. Required to compute motor RPM
2629 | Default | Min | Max |
2635 ### motor_pwm_protocol
2637 Protocol that is used to send motor updates to ESCs. Possible values - STANDARD, ONESHOT125, ONESHOT42, MULTISHOT, DSHOT150, DSHOT300, DSHOT600, DSHOT1200, BRUSHED
2639 | Default | Min | Max |
2647 Output frequency (in Hz) for motor pins. Applies only to brushed motors.
2649 | Default | Min | Max |
2651 | 16000 | 50 | 32000 |
2655 ### msp_override_channels
2657 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.
2659 | Default | Min | Max |
2669 | Default | Min | Max |
2671 | _empty_ | | MAX_NAME_LENGTH |
2675 ### nav_auto_climb_rate
2677 Maximum climb/descent rate that UAV is allowed to reach during navigation modes. [cm/s]
2679 | Default | Min | Max |
2685 ### nav_auto_disarm_delay
2687 Delay before craft disarms when `nav_disarm_on_landing` is set (ms)
2689 | Default | Min | Max |
2691 | 1000 | 100 | 10000 |
2697 Speed in fully autonomous modes (RTH, WP) [cm/s]. Used for WP mode when no specific WP speed set. [Multirotor only]
2699 | Default | Min | Max |
2705 ### nav_disarm_on_landing
2707 If set to ON, INAV disarms the FC after landing
2709 | Default | Min | Max |
2715 ### nav_emerg_landing_speed
2717 Rate of descent UAV will try to maintain when doing emergency descent sequence [cm/s]
2719 | Default | Min | Max |
2721 | 500 | 100 | 2000 |
2725 ### nav_extra_arming_safety
2727 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
2729 | Default | Min | Max |
2735 ### nav_fw_allow_manual_thr_increase
2737 Enable the possibility to manually increase the throttle in auto throttle controlled modes for fixed wing
2739 | Default | Min | Max |
2745 ### nav_fw_bank_angle
2747 Max roll angle when rolling / turning in GPS assisted modes, is also restrained by global max_angle_inclination_rll
2749 | Default | Min | Max |
2755 ### nav_fw_climb_angle
2757 Max pitch angle when climbing in GPS assisted modes, is also restrained by global max_angle_inclination_pit
2759 | Default | Min | Max |
2765 ### nav_fw_control_smoothness
2767 How smoothly the autopilot controls the airplane to correct the navigation error
2769 | Default | Min | Max |
2775 ### nav_fw_cruise_speed
2777 Speed for the plane/wing at cruise throttle used for remaining flight time/distance estimation in cm/s
2779 | Default | Min | Max |
2785 ### nav_fw_cruise_thr
2787 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 )
2789 | Default | Min | Max |
2791 | 1400 | 1000 | 2000 |
2795 ### nav_fw_cruise_yaw_rate
2797 Max YAW rate when NAV CRUISE mode is enabled (0=disable control via yaw stick) [dps]
2799 | Default | Min | Max |
2805 ### nav_fw_dive_angle
2807 Max negative pitch angle when diving in GPS assisted modes, is also restrained by global max_angle_inclination_pit
2809 | Default | Min | Max |
2815 ### nav_fw_heading_p
2817 P gain of Heading Hold controller (Fixedwing)
2819 | Default | Min | Max |
2825 ### nav_fw_land_dive_angle
2827 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
2829 | Default | Min | Max |
2835 ### nav_fw_launch_abort_deadband
2837 Launch 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.
2839 | Default | Min | Max |
2845 ### nav_fw_launch_accel
2847 Forward acceleration threshold for bungee launch of throw launch [cm/s/s], 1G = 981 cm/s/s
2849 | Default | Min | Max |
2851 | 1863 | 1000 | 20000 |
2855 ### nav_fw_launch_climb_angle
2857 Climb angle (attitude of model, not climb slope) for launch sequence (degrees), is also restrained by global max_angle_inclination_pit
2859 | Default | Min | Max |
2865 ### nav_fw_launch_detect_time
2867 Time for which thresholds have to breached to consider launch happened [ms]
2869 | Default | Min | Max |
2875 ### nav_fw_launch_end_time
2877 Time for the transition of throttle and pitch angle, between the launch state and the subsequent flight mode [ms]
2879 | Default | Min | Max |
2885 ### nav_fw_launch_idle_motor_delay
2887 Delay between raising throttle and motor starting at idle throttle (ms)
2889 | Default | Min | Max |
2895 ### nav_fw_launch_idle_thr
2897 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)
2899 | Default | Min | Max |
2901 | 1000 | 1000 | 2000 |
2905 ### nav_fw_launch_manual_throttle
2907 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).
2909 | Default | Min | Max |
2915 ### nav_fw_launch_max_altitude
2917 Altitude (centimeters) at which LAUNCH mode will be turned off and regular flight mode will take over [0-60000].
2919 | Default | Min | Max |
2925 ### nav_fw_launch_max_angle
2927 Max tilt angle (pitch/roll combined) to consider launch successful. Set to 180 to disable completely [deg]
2929 | Default | Min | Max |
2935 ### nav_fw_launch_min_time
2937 Allow launch mode to execute at least this time (ms) and ignore stick movements [0-60000].
2939 | Default | Min | Max |
2945 ### nav_fw_launch_motor_delay
2947 Delay between detected launch and launch sequence start and throttling up (ms)
2949 | Default | Min | Max |
2955 ### nav_fw_launch_spinup_time
2957 Time to bring power from minimum throttle to nav_fw_launch_thr - to avoid big stress on ESC and large torque from propeller
2959 | Default | Min | Max |
2965 ### nav_fw_launch_thr
2967 Launch throttle - throttle to be set during launch sequence (pwm units)
2969 | Default | Min | Max |
2971 | 1700 | 1000 | 2000 |
2975 ### nav_fw_launch_timeout
2977 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)
2979 | Default | Min | Max |
2985 ### nav_fw_launch_velocity
2987 Forward velocity threshold for swing-launch detection [cm/s]
2989 | Default | Min | Max |
2991 | 300 | 100 | 10000 |
2995 ### nav_fw_loiter_radius
2997 PosHold radius. 3000 to 7500 is a good value (30-75m) [cm]
2999 | Default | Min | Max |
3001 | 7500 | 0 | 30000 |
3007 Maximum throttle for flying wing in GPS assisted modes
3009 | Default | Min | Max |
3011 | 1700 | 1000 | 2000 |
3017 Minimum throttle for flying wing in GPS assisted modes
3019 | Default | Min | Max |
3021 | 1200 | 1000 | 2000 |
3025 ### nav_fw_pitch2thr
3027 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)
3029 | Default | Min | Max |
3035 ### nav_fw_pitch2thr_smoothing
3037 How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by pitch_to_throttle_thresh.
3039 | Default | Min | Max |
3045 ### nav_fw_pitch2thr_threshold
3047 Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees]
3049 | Default | Min | Max |
3055 ### nav_fw_pos_hdg_d
3057 D gain of heading trajectory PID controller. (Fixedwing, rovers, boats)
3059 | Default | Min | Max |
3065 ### nav_fw_pos_hdg_i
3067 I gain of heading trajectory PID controller. (Fixedwing, rovers, boats)
3069 | Default | Min | Max |
3075 ### nav_fw_pos_hdg_p
3077 P gain of heading PID controller. (Fixedwing, rovers, boats)
3079 | Default | Min | Max |
3085 ### nav_fw_pos_hdg_pidsum_limit
3087 Output limit for heading trajectory PID controller. (Fixedwing, rovers, boats)
3089 | Default | Min | Max |
3091 | 350 | PID_SUM_LIMIT_MIN | PID_SUM_LIMIT_MAX |
3097 D gain of 2D trajectory PID controller. Too high and there will be overshoot in trajectory. Better start tuning with zero
3099 | Default | Min | Max |
3107 I gain of 2D trajectory PID controller. Too high and there will be overshoot in trajectory. Better start tuning with zero
3109 | Default | Min | Max |
3117 P gain of 2D trajectory PID controller. Play with this to get a straight line between waypoints or a straight RTH
3119 | Default | Min | Max |
3127 D gain of altitude PID controller (Fixedwing)
3129 | Default | Min | Max |
3137 I gain of altitude PID controller (Fixedwing)
3139 | Default | Min | Max |
3147 P gain of altitude PID controller (Fixedwing)
3149 | Default | Min | Max |
3155 ### nav_fw_soaring_motor_stop
3157 Stops motor when Soaring mode enabled.
3159 | Default | Min | Max |
3165 ### nav_fw_soaring_pitch_deadband
3167 Pitch Angle deadband when soaring mode enabled (deg). Angle mode inactive within deadband allowing pitch to free float whilst soaring.
3169 | Default | Min | Max |
3175 ### nav_fw_wp_tracking_accuracy
3177 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.
3179 | Default | Min | Max |
3185 ### nav_fw_wp_tracking_max_angle
3187 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.
3189 | Default | Min | Max |
3195 ### nav_fw_wp_turn_smoothing
3197 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).
3199 | Default | Min | Max |
3205 ### nav_fw_yaw_deadband
3207 Deadband for heading trajectory PID controller. When heading error is below the deadband, controller assumes that vehicle is on course
3209 | Default | Min | Max |
3215 ### nav_land_detect_sensitivity
3217 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.
3219 | Default | Min | Max |
3225 ### nav_land_maxalt_vspd
3227 Vertical descent velocity above nav_land_slowdown_maxalt during the RTH landing phase. [cm/s]
3229 | Default | Min | Max |
3231 | 200 | 100 | 2000 |
3235 ### nav_land_minalt_vspd
3237 Vertical descent velocity under nav_land_slowdown_minalt during the RTH landing phase. [cm/s]
3239 | Default | Min | Max |
3245 ### nav_land_slowdown_maxalt
3247 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]
3249 | Default | Min | Max |
3251 | 2000 | 500 | 4000 |
3255 ### nav_land_slowdown_minalt
3257 Defines at what altitude the descent velocity should start to be `nav_land_minalt_vspd` [cm]
3259 | Default | Min | Max |
3265 ### nav_manual_climb_rate
3267 Maximum climb/descent rate firmware is allowed when processing pilot input for ALTHOLD control mode [cm/s]
3269 | Default | Min | Max |
3275 ### nav_manual_speed
3277 Maximum speed allowed when processing pilot input for POSHOLD/CRUISE control mode [cm/s] [Multirotor only]
3279 | Default | Min | Max |
3285 ### nav_max_altitude
3287 Max allowed altitude (above Home Point) that applies to all NAV modes (including Altitude Hold). 0 means limit is disabled
3289 | Default | Min | Max |
3295 ### nav_max_auto_speed
3297 Maximum speed allowed in fully autonomous modes (RTH, WP) [cm/s] [Multirotor only]
3299 | Default | Min | Max |
3301 | 1000 | 10 | 2000 |
3305 ### nav_max_terrain_follow_alt
3307 Max allowed above the ground altitude for terrain following mode
3309 | Default | Min | Max |
3315 ### nav_mc_bank_angle
3317 Maximum banking angle (deg) that multicopter navigation is allowed to set. Machine must be able to satisfy this angle without loosing altitude
3319 | Default | Min | Max |
3325 ### nav_mc_braking_bank_angle
3327 max angle that MR is allowed to bank in BOOST mode
3329 | Default | Min | Max |
3335 ### nav_mc_braking_boost_disengage_speed
3337 BOOST will be disabled when speed goes below this value
3339 | Default | Min | Max |
3345 ### nav_mc_braking_boost_factor
3347 acceleration factor for BOOST phase
3349 | Default | Min | Max |
3355 ### nav_mc_braking_boost_speed_threshold
3357 BOOST can be enabled when speed is above this value
3359 | Default | Min | Max |
3361 | 150 | 100 | 1000 |
3365 ### nav_mc_braking_boost_timeout
3367 how long in ms BOOST phase can happen
3369 | Default | Min | Max |
3375 ### nav_mc_braking_disengage_speed
3377 braking is disabled when speed goes below this value
3379 | Default | Min | Max |
3385 ### nav_mc_braking_speed_threshold
3387 min speed in cm/s above which braking can happen
3389 | Default | Min | Max |
3395 ### nav_mc_braking_timeout
3397 timeout in ms for braking
3399 | Default | Min | Max |
3401 | 2000 | 100 | 5000 |
3405 ### nav_mc_heading_p
3407 P gain of Heading Hold controller (Multirotor)
3409 | Default | Min | Max |
3415 ### nav_mc_hover_thr
3417 Multicopter hover throttle hint for altitude controller. Should be set to approximate throttle value when drone is hovering.
3419 | Default | Min | Max |
3421 | 1500 | 1000 | 2000 |
3425 ### nav_mc_pos_deceleration_time
3427 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
3429 | Default | Min | Max |
3437 Expo for PosHold control
3439 | Default | Min | Max |
3447 Controls how fast the drone will fly towards the target position. This is a multiplier to convert displacement to target velocity
3449 | Default | Min | Max |
3457 P gain of altitude PID controller (Multirotor)
3459 | Default | Min | Max |
3467 D gain of Position-Rate (Velocity to Acceleration) PID controller. It can damp P and I. Increasing D might help when drone overshoots target.
3469 | Default | Min | Max |
3475 ### nav_mc_vel_xy_dterm_attenuation
3477 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.
3479 | Default | Min | Max |
3485 ### nav_mc_vel_xy_dterm_attenuation_end
3487 A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation reaches maximum
3489 | Default | Min | Max |
3495 ### nav_mc_vel_xy_dterm_attenuation_start
3497 A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation begins
3499 | Default | Min | Max |
3505 ### nav_mc_vel_xy_dterm_lpf_hz
3509 | Default | Min | Max |
3515 ### nav_mc_vel_xy_ff
3519 | Default | Min | Max |
3527 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
3529 | Default | Min | Max |
3537 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
3539 | Default | Min | Max |
3547 D gain of velocity PID controller
3549 | Default | Min | Max |
3557 I gain of velocity PID controller
3559 | Default | Min | Max |
3567 P gain of velocity PID controller
3569 | Default | Min | Max |
3575 ### nav_mc_wp_slowdown
3577 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.
3579 | Default | Min | Max |
3585 ### nav_min_rth_distance
3587 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.
3589 | Default | Min | Max |
3595 ### nav_mission_planner_reset
3597 With Reset ON WP Mission Planner waypoint count can be reset to 0 by toggling the mode switch ON-OFF-ON.
3599 | Default | Min | Max |
3605 ### nav_overrides_motor_stop
3607 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
3609 | Default | Min | Max |
3615 ### nav_position_timeout
3617 If GPS fails wait for this much seconds before switching to emergency landing mode (0 - disable)
3619 | Default | Min | Max |
3625 ### nav_rth_abort_threshold
3627 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]
3629 | Default | Min | Max |
3631 | 50000 | 0 | 65000 |
3635 ### nav_rth_allow_landing
3637 If set to ON drone will land as a last phase of RTH.
3639 | Default | Min | Max |
3645 ### nav_rth_alt_control_override
3647 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)
3649 | Default | Min | Max |
3655 ### nav_rth_alt_mode
3657 Configure how the aircraft will manage altitude on the way home, see Navigation modes on wiki for more details
3659 | Default | Min | Max |
3665 ### nav_rth_altitude
3667 Used in EXTRA, FIXED and AT_LEAST rth alt modes [cm] (Default 1000 means 10 meters)
3669 | Default | Min | Max |
3675 ### nav_rth_climb_first
3677 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)
3679 | Default | Min | Max |
3685 ### nav_rth_climb_first_stage_altitude
3687 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.
3689 | Default | Min | Max |
3695 ### nav_rth_climb_first_stage_mode
3697 This determines how rth_climb_first_stage_altitude is used. Default is AT_LEAST.
3699 | Default | Min | Max |
3705 ### nav_rth_climb_ignore_emerg
3707 If set to ON, aircraft will execute initial climb regardless of position sensor (GPS) status.
3709 | Default | Min | Max |
3715 ### nav_rth_home_altitude
3717 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]
3719 | Default | Min | Max |
3725 ### nav_rth_tail_first
3727 If set to ON drone will return tail-first. Obviously meaningless for airplanes.
3729 | Default | Min | Max |
3735 ### nav_rth_trackback_distance
3737 Maximum distance allowed for RTH trackback. Normal RTH is executed once this distance is exceeded [m].
3739 | Default | Min | Max |
3745 ### nav_rth_trackback_mode
3747 Useage modes for RTH Trackback. OFF = disabled, ON = Normal and Failsafe RTH, FS = Failsafe RTH only.
3749 | Default | Min | Max |
3755 ### nav_use_fw_yaw_control
3757 Enables or Disables the use of the heading PID controller on fixed wing. Heading PID controller is always enabled for rovers and boats
3759 | Default | Min | Max |
3765 ### nav_use_midthr_for_althold
3767 If set to OFF, the FC remembers your throttle stick position when enabling ALTHOLD and treats it as a neutral midpoint for holding altitude
3769 | Default | Min | Max |
3775 ### nav_user_control_mode
3777 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.
3779 | Default | Min | Max |
3785 ### nav_wp_enforce_altitude
3787 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.
3789 | Default | Min | Max |
3795 ### nav_wp_load_on_boot
3797 If set to ON, waypoints will be automatically loaded from EEPROM to the FC during startup.
3799 | Default | Min | Max |
3805 ### nav_wp_max_safe_distance
3807 First waypoint in the mission should be closer than this value [m]. A value of 0 disables this check.
3809 | Default | Min | Max |
3815 ### nav_wp_mission_restart
3817 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.
3819 | Default | Min | Max |
3825 ### nav_wp_multi_mission_index
3827 Index of active mission selected from multi mission WP entry loaded in flight controller. Limited to a maximum of 9 missions.
3829 | Default | Min | Max |
3837 Waypoint radius [cm]. Waypoint would be considered reached if machine is within this radius
3839 | Default | Min | Max |
3841 | 100 | 10 | 10000 |
3847 Selection of OPFLOW hardware.
3849 | Default | Min | Max |
3859 | Default | Min | Max |
3861 | 10.5 | 0 | 10000 |
3865 ### osd_ahi_bordered
3867 Shows a border/corners around the AHI region (pixel OSD only)
3869 | Default | Min | Max |
3875 ### osd_ahi_camera_uptilt_comp
3877 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).
3879 | Default | Min | Max |
3887 AHI height in pixels (pixel OSD only)
3889 | Default | Min | Max |
3895 ### osd_ahi_max_pitch
3897 Max pitch, in degrees, for OSD artificial horizon
3899 | Default | Min | Max |
3905 ### osd_ahi_pitch_interval
3907 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)
3909 | Default | Min | Max |
3915 ### osd_ahi_reverse_roll
3917 Switches the artificial horizon in the OSD to instead be a bank indicator, by reversing the direction of its movement.
3919 | Default | Min | Max |
3927 Sets OSD Artificial Horizon style "DEFAULT" or "LINE" for the FrSky Graphical OSD.
3929 | Default | Min | Max |
3935 ### osd_ahi_vertical_offset
3937 AHI vertical offset from center (pixel OSD only)
3939 | Default | Min | Max |
3941 | -18 | -128 | 127 |
3947 AHI width in pixels (pixel OSD only)
3949 | Default | Min | Max |
3955 ### osd_airspeed_alarm_max
3957 Airspeed above which the airspeed OSD element will start blinking (cm/s)
3959 | Default | Min | Max |
3965 ### osd_airspeed_alarm_min
3967 Airspeed under which the airspeed OSD element will start blinking (cm/s)
3969 | Default | Min | Max |
3977 Value above which to make the OSD relative altitude indicator blink (meters)
3979 | Default | Min | Max |
3985 ### osd_baro_temp_alarm_max
3987 Temperature above which the baro temperature OSD element will start blinking (decidegrees centigrade)
3989 | Default | Min | Max |
3991 | 600 | -550 | 1250 |
3995 ### osd_baro_temp_alarm_min
3997 Temperature under which the baro temperature OSD element will start blinking (decidegrees centigrade)
3999 | Default | Min | Max |
4001 | -200 | -550 | 1250 |
4005 ### osd_camera_fov_h
4007 Horizontal field of view for the camera in degres
4009 | Default | Min | Max |
4015 ### osd_camera_fov_v
4017 Vertical field of view for the camera in degres
4019 | Default | Min | Max |
4025 ### osd_camera_uptilt
4027 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).
4029 | Default | Min | Max |
4035 ### osd_coordinate_digits
4039 | Default | Min | Max |
4045 ### osd_crosshairs_style
4047 To set the visual type for the crosshair
4049 | Default | Min | Max |
4055 ### osd_crsf_lq_format
4059 | Default | Min | Max |
4065 ### osd_current_alarm
4067 Value above which the OSD current consumption element will start blinking. Measured in full Amperes.
4069 | Default | Min | Max |
4077 Value above which to make the OSD distance from home indicator blink (meters)
4079 | Default | Min | Max |
4081 | 1000 | 0 | 50000 |
4085 ### osd_esc_rpm_precision
4087 Number of characters used to display the RPM value.
4089 | Default | Min | Max |
4095 ### osd_esc_temp_alarm_max
4097 Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade)
4099 | Default | Min | Max |
4101 | 900 | -550 | 1500 |
4105 ### osd_esc_temp_alarm_min
4107 Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade)
4109 | Default | Min | Max |
4111 | -200 | -550 | 1500 |
4115 ### osd_estimations_wind_compensation
4117 Use wind estimation for remaining flight time/distance estimation
4119 | Default | Min | Max |
4125 ### osd_failsafe_switch_layout
4127 If enabled the OSD automatically switches to the first layout during failsafe
4129 | Default | Min | Max |
4137 Force OSD to work in grid mode even if the OSD device supports pixel level access (mainly used for development)
4139 | Default | Min | Max |
4145 ### osd_gforce_alarm
4147 Value above which the OSD g force indicator will blink (g)
4149 | Default | Min | Max |
4155 ### osd_gforce_axis_alarm_max
4157 Value above which the OSD axis g force indicators will blink (g)
4159 | Default | Min | Max |
4165 ### osd_gforce_axis_alarm_min
4167 Value under which the OSD axis g force indicators will blink (g)
4169 | Default | Min | Max |
4175 ### osd_home_position_arm_screen
4177 Should home position coordinates be displayed on the arming screen.
4179 | Default | Min | Max |
4185 ### osd_horizon_offset
4187 To vertically adjust the whole OSD and AHI and scrolling bars
4189 | Default | Min | Max |
4195 ### osd_hud_homepoint
4197 To 3D-display the home point location in the hud
4199 | Default | Min | Max |
4207 To display little arrows around the crossair showing where the home point is in the hud
4209 | Default | Min | Max |
4215 ### osd_hud_margin_h
4217 Left and right margins for the hud area
4219 | Default | Min | Max |
4225 ### osd_hud_margin_v
4227 Top and bottom margins for the hud area
4229 | Default | Min | Max |
4235 ### osd_hud_radar_alt_difference_display_time
4237 Time in seconds to display the altitude difference in radar
4239 | Default | Min | Max |
4245 ### osd_hud_radar_disp
4247 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
4249 | Default | Min | Max |
4255 ### osd_hud_radar_distance_display_time
4257 Time in seconds to display the distance in radar
4259 | Default | Min | Max |
4265 ### osd_hud_radar_range_max
4267 In meters, radar aircrafts further away than this will not be displayed in the hud
4269 | Default | Min | Max |
4271 | 4000 | 100 | 9990 |
4275 ### osd_hud_radar_range_min
4277 In meters, radar aircrafts closer than this will not be displayed in the hud
4279 | Default | Min | Max |
4287 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)
4289 | Default | Min | Max |
4295 ### osd_imu_temp_alarm_max
4297 Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade)
4299 | Default | Min | Max |
4301 | 600 | -550 | 1250 |
4305 ### osd_imu_temp_alarm_min
4307 Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade)
4309 | Default | Min | Max |
4311 | -200 | -550 | 1250 |
4315 ### osd_left_sidebar_scroll
4319 | Default | Min | Max |
4325 ### osd_left_sidebar_scroll_step
4327 How many units each sidebar step represents. 0 means the default value for the scroll type.
4329 | Default | Min | Max |
4335 ### osd_link_quality_alarm
4337 LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%
4339 | Default | Min | Max |
4345 ### osd_mah_used_precision
4347 Number of digits used to display mAh used.
4349 | Default | Min | Max |
4355 ### osd_main_voltage_decimals
4357 Number of decimals for the battery voltages displayed in the OSD [1-2].
4359 | Default | Min | Max |
4365 ### osd_msp_displayport_fullframe_interval
4367 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)
4369 | Default | Min | Max |
4375 ### osd_neg_alt_alarm
4377 Value below which (negative altitude) to make the OSD relative altitude indicator blink (meters)
4379 | Default | Min | Max |
4385 ### osd_pan_servo_index
4387 Index of the pan servo to adjust osd home heading direction based on camera pan. Note that this feature does not work with continiously rotating servos.
4389 | Default | Min | Max |
4395 ### osd_pan_servo_pwm2centideg
4397 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.
4399 | Default | Min | Max |
4405 ### osd_plus_code_digits
4407 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.
4409 | Default | Min | Max |
4415 ### osd_plus_code_short
4417 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.
4419 | Default | Min | Max |
4425 ### osd_right_sidebar_scroll
4429 | Default | Min | Max |
4435 ### osd_right_sidebar_scroll_step
4437 Same as left_sidebar_scroll_step, but for the right sidebar
4439 | Default | Min | Max |
4445 ### osd_row_shiftdown
4447 Number of rows to shift the OSD display (increase if top rows are cut off)
4449 | Default | Min | Max |
4457 Value below which to make the OSD RSSI indicator blink
4459 | Default | Min | Max |
4465 ### osd_rssi_dbm_alarm
4467 RSSI dBm indicator blinks below this value [dBm]. 0 disables this alarm
4469 | Default | Min | Max |
4475 ### osd_rssi_dbm_max
4477 RSSI dBm upper end of curve. Perfect rssi (max) = 100%
4479 | Default | Min | Max |
4485 ### osd_rssi_dbm_min
4487 RSSI dBm lower end of curve or RX sensitivity level. Worst rssi (min) = 0%
4489 | Default | Min | Max |
4495 ### osd_sidebar_height
4497 Height of sidebars in rows. 0 leaves only the level indicator arrows (Not for pixel OSD)
4499 | Default | Min | Max |
4505 ### osd_sidebar_horizontal_offset
4507 Sidebar horizontal offset from default position. Positive values move the sidebars closer to the edges.
4509 | Default | Min | Max |
4515 ### osd_sidebar_scroll_arrows
4519 | Default | Min | Max |
4527 Value below which Crossfire SNR Alarm pops-up. (dB)
4529 | Default | Min | Max |
4535 ### osd_speed_source
4537 Sets the speed type displayed by the DJI OSD and OSD canvas (FrSky Pixel): GROUND, 3D, AIR
4539 | Default | Min | Max |
4545 ### osd_stats_energy_unit
4547 Unit used for the drawn energy in the OSD stats [MAH/WH] (milliAmpere hour/ Watt hour)
4549 | Default | Min | Max |
4555 ### osd_stats_min_voltage_unit
4557 Display minimum voltage of the `BATTERY` or the average per `CELL` in the OSD stats.
4559 | Default | Min | Max |
4565 ### osd_stats_page_auto_swap_time
4567 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.
4569 | Default | Min | Max |
4575 ### osd_switch_indicator_one_channel
4577 RC Channel to use for OSD switch indicator 1.
4579 | Default | Min | Max |
4581 | 5 | 5 | MAX_SUPPORTED_RC_CHANNEL_COUNT |
4585 ### osd_switch_indicator_one_name
4587 Character to use for OSD switch incicator 1.
4589 | Default | Min | Max |
4595 ### osd_switch_indicator_three_channel
4597 RC Channel to use for OSD switch indicator 3.
4599 | Default | Min | Max |
4601 | 5 | 5 | MAX_SUPPORTED_RC_CHANNEL_COUNT |
4605 ### osd_switch_indicator_three_name
4607 Character to use for OSD switch incicator 3.
4609 | Default | Min | Max |
4615 ### osd_switch_indicator_two_channel
4617 RC Channel to use for OSD switch indicator 2.
4619 | Default | Min | Max |
4621 | 5 | 5 | MAX_SUPPORTED_RC_CHANNEL_COUNT |
4625 ### osd_switch_indicator_two_name
4627 Character to use for OSD switch incicator 2.
4629 | Default | Min | Max |
4635 ### osd_switch_indicator_zero_channel
4637 RC Channel to use for OSD switch indicator 0.
4639 | Default | Min | Max |
4641 | 5 | 5 | MAX_SUPPORTED_RC_CHANNEL_COUNT |
4645 ### osd_switch_indicator_zero_name
4647 Character to use for OSD switch incicator 0.
4649 | Default | Min | Max |
4655 ### osd_switch_indicators_align_left
4657 Align text to left of switch indicators
4659 | Default | Min | Max |
4665 ### osd_system_msg_display_time
4667 System message display cycle time for multiple messages (milliseconds).
4669 | Default | Min | Max |
4671 | 1000 | 500 | 5000 |
4677 To enable OSD telemetry for antenna tracker. Possible values are `OFF`, `ON` and `TEST`
4679 | Default | Min | Max |
4685 ### osd_temp_label_align
4687 Allows to chose between left and right alignment for the OSD temperature sensor labels. Valid values are `LEFT` and `RIGHT`
4689 | Default | Min | Max |
4697 Value above which to make the OSD flight time indicator blink (minutes)
4699 | Default | Min | Max |
4707 IMPERIAL, METRIC, UK
4709 | Default | Min | Max |
4715 ### osd_video_system
4717 Video system used. Possible values are `AUTO`, `PAL`, `NTSC`, `HDZERO`, 'DJIWTF', 'AVATAR' and `BF43COMPAT`
4719 | Default | Min | Max |
4727 Output function assignment mode. AUTO assigns outputs according to the default mapping, SERVOS assigns all outputs to servos, MOTORS assigns all outputs to motors
4729 | Default | Min | Max |
4737 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`
4739 | Default | Min | Max |
4747 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
4749 | Default | Min | Max |
4751 | 500 | PID_SUM_LIMIT_MIN | PID_SUM_LIMIT_MAX |
4755 ### pidsum_limit_yaw
4757 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
4759 | Default | Min | Max |
4761 | 350 | PID_SUM_LIMIT_MIN | PID_SUM_LIMIT_MAX |
4769 | Default | Min | Max |
4771 | _empty_ | | MAX_NAME_LENGTH |
4777 Mode assignment for PINIO#1
4779 | Default | Min | Max |
4781 | `BOX_PERMANENT_ID_NONE` | 0 | 255 |
4787 Mode assignment for PINIO#1
4789 | Default | Min | Max |
4791 | `BOX_PERMANENT_ID_NONE` | 0 | 255 |
4797 Mode assignment for PINIO#1
4799 | Default | Min | Max |
4801 | `BOX_PERMANENT_ID_NONE` | 0 | 255 |
4807 Mode assignment for PINIO#1
4809 | Default | Min | Max |
4811 | `BOX_PERMANENT_ID_NONE` | 0 | 255 |
4817 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.
4819 | Default | Min | Max |
4827 Selection of pitot hardware.
4829 | Default | Min | Max |
4835 ### pitot_lpf_milli_hz
4839 | Default | Min | Max |
4849 | Default | Min | Max |
4857 Defines UAV platform type. Allowed values: "MULTIROTOR", "AIRPLANE", "HELICOPTER", "TRICOPTER", "ROVER", "BOAT". Currently only MULTIROTOR, AIRPLANE and TRICOPTER types are implemented
4859 | Default | Min | Max |
4865 ### pos_hold_deadband
4867 Stick deadband in [r/c points], applied after r/c deadband and expo. Used for adjustments in navigation modes.
4869 | Default | Min | Max |
4877 Duration (ms) for which Prearm being activated is valid. after this, Prearm needs to be reset. 0 means Prearm does not timeout.
4879 | Default | Min | Max |
4881 | 10000 | 0 | 10000 |
4885 ### rangefinder_hardware
4887 Selection of rangefinder hardware.
4889 | Default | Min | Max |
4895 ### rangefinder_median_filter
4897 3-point median filtering for rangefinder readouts
4899 | Default | Min | Max |
4905 ### rate_accel_limit_roll_pitch
4907 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.
4909 | Default | Min | Max |
4915 ### rate_accel_limit_yaw
4917 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.
4919 | Default | Min | Max |
4921 | 10000 | | 500000 |
4925 ### rate_dynamics_center_correction
4927 The center stick correction for Rate Dynamics
4929 | Default | Min | Max |
4935 ### rate_dynamics_center_sensitivity
4937 The center stick sensitivity for Rate Dynamics
4939 | Default | Min | Max |
4945 ### rate_dynamics_center_weight
4947 The center stick weight for Rate Dynamics
4949 | Default | Min | Max |
4955 ### rate_dynamics_end_correction
4957 The end stick correction for Rate Dynamics
4959 | Default | Min | Max |
4965 ### rate_dynamics_end_sensitivity
4967 The end stick sensitivity for Rate Dynamics
4969 | Default | Min | Max |
4975 ### rate_dynamics_end_weight
4977 The end stick weight for Rate Dynamics
4979 | Default | Min | Max |
4987 Exposition value used for the PITCH/ROLL axes by all the stabilized flights modes (all but `MANUAL`)
4989 | Default | Min | Max |
4997 When enabled, INAV will set RC filtering based on refresh rate and smoothing factor.
4999 | Default | Min | Max |
5005 ### rc_filter_lpf_hz
5007 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
5009 | Default | Min | Max |
5015 ### rc_filter_smoothing_factor
5017 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
5019 | Default | Min | Max |
5027 Exposition value used for the YAW axis by all the stabilized flights modes (all but `MANUAL`)
5029 | Default | Min | Max |
5035 ### reboot_character
5037 Special character used to trigger reboot
5039 | Default | Min | Max |
5047 Selection of receiver (RX) type. Additional configuration of a `serialrx_provider` and a UART will be needed for `SERIAL`
5049 | Default | Min | Max |
5051 | _target default_ | | |
5055 ### report_cell_voltage
5057 S.Port, D-Series, and IBUS telemetry: Send the average cell voltage if set to ON
5059 | Default | Min | Max |
5067 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.
5069 | Default | Min | Max |
5075 ### rpm_gyro_filter_enabled
5077 Enables gyro RPM filtere. Set to `ON` only when ESC telemetry is working and rotation speed of the motors is correctly reported to INAV
5079 | Default | Min | Max |
5085 ### rpm_gyro_harmonics
5087 Number of harmonic frequences to be covered by gyro RPM filter. Default value of `1` usually works just fine
5089 | Default | Min | Max |
5097 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`
5099 | Default | Min | Max |
5107 Q factor for gyro RPM filter. Lower values give softer, wider attenuation. Usually there is no need to change this setting
5109 | Default | Min | Max |
5115 ### rssi_adc_channel
5117 ADC channel to use for analog RSSI input. Defaults to board RSSI input (if available). 0 = disabled
5119 | Default | Min | Max |
5121 | _target default_ | ADC_CHN_NONE | ADC_CHN_MAX |
5127 RX channel containing the RSSI signal
5129 | Default | Min | Max |
5131 | 0 | 0 | MAX_SUPPORTED_RC_CHANNEL_COUNT |
5137 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.
5139 | Default | Min | Max |
5141 | 100 | RSSI_VISIBLE_VALUE_MIN | RSSI_VISIBLE_VALUE_MAX |
5147 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).
5149 | Default | Min | Max |
5151 | 0 | RSSI_VISIBLE_VALUE_MIN | RSSI_VISIBLE_VALUE_MAX |
5157 Source of RSSI input. Possible values: `NONE`, `AUTO`, `ADC`, `CHANNEL`, `PROTOCOL`, `MSP`
5159 | Default | Min | Max |
5165 ### rth_energy_margin
5167 Energy margin wanted after getting home (percent of battery energy capacity). Use for the remaining flight time/distance calculation
5169 | Default | Min | Max |
5177 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.
5179 | Default | Min | Max |
5181 | 2115 | PWM_PULSE_MIN | PWM_PULSE_MAX |
5187 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.
5189 | Default | Min | Max |
5191 | 885 | PWM_PULSE_MIN | PWM_PULSE_MAX |
5195 ### safehome_max_distance
5197 In order for a safehome to be used, it must be less than this distance (in cm) from the arming point.
5199 | Default | Min | Max |
5201 | 20000 | 0 | 65000 |
5205 ### safehome_usage_mode
5207 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.
5209 | Default | Min | Max |
5215 ### sbus_sync_interval
5219 | Default | Min | Max |
5221 | 3000 | 500 | 10000 |
5225 ### sdcard_detect_inverted
5227 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.
5229 | Default | Min | Max |
5231 | _target default_ | | |
5235 ### serialrx_halfduplex
5237 Allow serial receiver to operate on UART TX pin. With some receivers will allow control and telemetry over a single wire.
5239 | Default | Min | Max |
5245 ### serialrx_inverted
5247 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).
5249 | Default | Min | Max |
5255 ### serialrx_provider
5257 When feature SERIALRX is enabled, this allows connection to several receivers which output data via digital interface resembling serial. See RX section.
5259 | Default | Min | Max |
5261 | _target default_ | | |
5265 ### servo_autotrim_rotation_limit
5267 Servo midpoints are only updated when total aircraft rotation is less than this threshold [deg/s]. Only applies when using `feature FW_AUTOTRIM`.
5269 | Default | Min | Max |
5275 ### servo_center_pulse
5279 | Default | Min | Max |
5281 | 1500 | PWM_RANGE_MIN | PWM_RANGE_MAX |
5287 Selects the servo PWM output cutoff frequency. Value is in [Hz]
5289 | Default | Min | Max |
5297 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)
5299 | Default | Min | Max |
5307 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.
5309 | Default | Min | Max |
5315 ### setpoint_kalman_enabled
5317 Enable Kalman filter on the gyro data
5319 | Default | Min | Max |
5325 ### setpoint_kalman_q
5327 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
5329 | Default | Min | Max |
5335 ### sim_ground_station_number
5337 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.
5339 | Default | Min | Max |
5345 ### sim_low_altitude
5347 Threshold for low altitude warning messages sent by SIM module when the 'L' transmit flag is set in `sim_transmit_flags`.
5349 | Default | Min | Max |
5351 | -32767 | -32768 | 32767 |
5357 PIN code for the SIM module
5359 | Default | Min | Max |
5365 ### sim_transmit_flags
5367 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`
5369 | Default | Min | Max |
5371 | `SIM_TX_FLAG_FAILSAFE` | | 63 |
5375 ### sim_transmit_interval
5377 Text message transmission interval in seconds for SIM module. Minimum value: 10
5379 | Default | Min | Max |
5381 | 60 | SIM_MIN_TRANSMIT_INTERVAL | 65535 |
5387 If the aircraft tilt angle exceed this value the copter will refuse to arm.
5389 | Default | Min | Max |
5395 ### smartport_fuel_unit
5397 S.Port telemetry only: Unit of the value sent with the `FUEL` ID (FrSky D-Series always sends percent). [PERCENT/MAH/MWH]
5399 | Default | Min | Max |
5405 ### smartport_master_halfduplex
5409 | Default | Min | Max |
5415 ### smartport_master_inverted
5419 | Default | Min | Max |
5425 ### smith_predictor_delay
5427 Expected delay of the gyro signal. In milliseconds
5429 | Default | Min | Max |
5435 ### smith_predictor_lpf_hz
5437 Cutoff frequency for the Smith Predictor Low Pass Filter
5439 | Default | Min | Max |
5445 ### smith_predictor_strength
5447 The strength factor of a Smith Predictor of PID measurement. In percents
5449 | Default | Min | Max |
5455 ### spektrum_sat_bind
5457 0 = disabled. Used to bind the spektrum satellite to RX
5459 | Default | Min | Max |
5461 | `SPEKTRUM_SAT_BIND_DISABLED` | SPEKTRUM_SAT_BIND_DISABLED | SPEKTRUM_SAT_BIND_MAX |
5469 | Default | Min | Max |
5479 | Default | Min | Max |
5487 General switch of the statistics recording feature (a.k.a. odometer)
5489 | Default | Min | Max |
5495 ### stats_total_dist
5497 Total flight distance [in meters]. The value is updated on every disarm when "stats" are enabled.
5499 | Default | Min | Max |
5501 | 0 | | 2147483647 |
5505 ### stats_total_energy
5507 Total energy consumption [in mWh]. The value is updated on every disarm when "stats" are enabled.
5509 | Default | Min | Max |
5511 | 0 | | 2147483647 |
5515 ### stats_total_time
5517 Total flight time [in seconds]. The value is updated on every disarm when "stats" are enabled.
5519 | Default | Min | Max |
5521 | 0 | | 2147483647 |
5525 ### switch_disarm_delay
5527 Delay before disarming when requested by switch (ms) [0-1000]
5529 | Default | Min | Max |
5535 ### telemetry_halfduplex
5537 S.Port telemetry only: Turn UART into UNIDIR for usage on F1 and F4 target. See Telemetry.md for details
5539 | Default | Min | Max |
5545 ### telemetry_inverted
5547 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.
5549 | Default | Min | Max |
5555 ### telemetry_switch
5557 Which aux channel to use to change serial output & baud rate (MSP / Telemetry). It disables automatic switching to Telemetry when armed.
5559 | Default | Min | Max |
5567 Weight used for the throttle compensation based on battery voltage. See the [battery documentation](Battery.md#automatic-throttle-compensation-based-on-battery-voltage)
5569 | Default | Min | Max |
5577 Throttle exposition value
5579 | Default | Min | Max |
5587 Throttle value when the stick is set to mid-position. Used in the throttle curve calculation.
5589 | Default | Min | Max |
5597 The percentage of the throttle range (`max_throttle` - `min_command`) above `min_command` used for minimum / idle throttle.
5599 | Default | Min | Max |
5607 Throttle scaling factor. `1` means no throttle scaling. `0.5` means throttle scaled down by 50%
5609 | Default | Min | Max |
5615 ### throttle_tilt_comp_str
5617 Can be used in ANGLE and HORIZON mode and will automatically boost throttle when banking. Setting is in percentage, 0=disabled.
5619 | Default | Min | Max |
5629 | Default | Min | Max |
5631 | 1500 | PWM_RANGE_MIN | PWM_RANGE_MAX |
5637 Throttle PID attenuation reduces influence of P on ROLL and PITCH as throttle increases. For every 1% throttle after the TPA breakpoint, P is reduced by the TPA rate.
5639 | Default | Min | Max |
5645 ### tri_unarmed_servo
5647 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.
5649 | Default | Min | Max |
5655 ### turtle_mode_power_factor
5657 Turtle mode power factor
5659 | Default | Min | Max |
5665 ### tz_automatic_dst
5667 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`.
5669 | Default | Min | Max |
5677 Time zone offset from UTC, in minutes. This is applied to the GPS time for logging and time-stamping of Blackbox logs
5679 | Default | Min | Max |
5685 ### vbat_adc_channel
5687 ADC channel to use for battery voltage sensor. Defaults to board VBAT input (if available). 0 = disabled
5689 | Default | Min | Max |
5691 | _target default_ | ADC_CHN_NONE | ADC_CHN_MAX |
5695 ### vbat_cell_detect_voltage
5697 Maximum voltage per cell, used for auto-detecting the number of cells of the battery in 0.01V units.
5699 | Default | Min | Max |
5705 ### vbat_max_cell_voltage
5707 Maximum voltage per cell in 0.01V units, default is 4.20V
5709 | Default | Min | Max |
5717 Vbat voltage source. Possible values: `NONE`, `ADC`, `ESC`. `ESC` required ESC telemetry enebled and running
5719 | Default | Min | Max |
5725 ### vbat_min_cell_voltage
5727 Minimum voltage per cell, this triggers battery out alarms, in 0.01V units, default is 330 (3.3V)
5729 | Default | Min | Max |
5737 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.
5739 | Default | Min | Max |
5741 | _target default_ | 0 | 65535 |
5745 ### vbat_warning_cell_voltage
5747 Warning voltage per cell, this triggers battery-warning alarms, in 0.01V units, default is 350 (3.5V)
5749 | Default | Min | Max |
5757 Configure the VTX band. Set to zero to use `vtx_freq`. Bands: 1: A, 2: B, 3: E, 4: F, 5: Race.
5759 | Default | Min | Max |
5761 | 1 | VTX_SETTINGS_NO_BAND | VTX_SETTINGS_MAX_BAND |
5767 Channel to use within the configured `vtx_band`. Valid values are [1, 8].
5769 | Default | Min | Max |
5771 | 1 | VTX_SETTINGS_MIN_CHANNEL | VTX_SETTINGS_MAX_CHANNEL |
5775 ### vtx_frequency_group
5777 VTx Frequency group to use. Frequency groups: FREQUENCYGROUP_5G8: 5.8GHz, FREQUENCYGROUP_2G4: 2.4GHz, FREQUENCYGROUP_1G3: 1.3GHz.
5779 | Default | Min | Max |
5781 | FREQUENCYGROUP_5G8 | 0 | 2 |
5787 Use half duplex UART to communicate with the VTX, using only a TX pin in the FC.
5789 | Default | Min | Max |
5795 ### vtx_low_power_disarm
5797 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.
5799 | Default | Min | Max |
5805 ### vtx_max_power_override
5807 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
5809 | Default | Min | Max |
5815 ### vtx_pit_mode_chan
5819 | Default | Min | Max |
5821 | 1 | VTX_SETTINGS_MIN_CHANNEL | VTX_SETTINGS_MAX_CHANNEL |
5827 VTX RF power level to use. The exact number of mw depends on the VTX hardware.
5829 | Default | Min | Max |
5831 | 1 | VTX_SETTINGS_MIN_POWER | VTX_SETTINGS_MAX_POWER |
5835 ### vtx_smartaudio_alternate_softserial_method
5837 Enable the alternate softserial method. This is the method used in INAV 3.0 and ealier.
5839 | Default | Min | Max |
5845 ### vtx_smartaudio_early_akk_workaround
5847 Enable workaround for early AKK SAudio-enabled VTX bug.
5849 | Default | Min | Max |
5855 ### vtx_smartaudio_stopbits
5857 Set stopbit count for serial (TBS Sixty9 SmartAudio 2.1 require value of 1 bit)
5859 | Default | Min | Max |
5865 ### vtx_softserial_shortstop
5867 Enable the 3x shorter stopbit on softserial. Need for some IRC Tramp VTXes.
5869 | Default | Min | Max |
5877 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.
5879 | Default | Min | Max |
5887 Yaw P term low pass filter cutoff frequency. Should be disabled (set to `0`) on small multirotors (7 inches and below)
5889 | Default | Min | Max |
5897 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.
5899 | Default | Min | Max |