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Merge branch 'master' into abo_waypoint_tracking

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breadoven 2022-08-12 13:02:36 +01:00 • committed by GitHub
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docs/Settings.md
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@ -362,16 +362,6 @@ Selection of baro hardware. See Wiki Sensor auto detect and hardware failure det
---
### baro_median_filter
3-point median filtering for barometer readouts. No reason to change this setting
| Default | Min | Max |
| --- | --- | --- |
| ON | OFF | ON |
---
### bat_cells
Number of cells of the battery (0 = auto-detect), see battery documentation. 7S, 9S and 11S batteries cannot be auto-detected.
@ -762,6 +752,16 @@ Defines the type of stage 1 D-term LPF filter. Possible values: `PT1`, `BIQUAD`,
---
### dynamic_gyro_notch_3d_q
Q factor for 3D dynamic notches
| Default | Min | Max |
| --- | --- | --- |
| 200 | 1 | 1000 |
---
### dynamic_gyro_notch_enabled
Enable/disable dynamic gyro notch also known as Matrix Filter
@ -782,6 +782,16 @@ Minimum frequency for dynamic notches. Default value of `150` works best with 5"
---
### dynamic_gyro_notch_mode
Gyro dynamic notch type
| Default | Min | Max |
| --- | --- | --- |
| 2D | | |
---
### dynamic_gyro_notch_q
Q factor for dynamic notches
@ -2952,6 +2962,16 @@ Dive angle that airplane will use during final landing phase. During dive phase,
---
### nav_fw_launch_abort_deadband
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.
| Default | Min | Max |
| --- | --- | --- |
| 100 | 2 | 250 |
---
### nav_fw_launch_accel
Forward acceleration threshold for bungee launch of throw launch [cm/s/s], 1G = 981 cm/s/s
@ -3012,6 +3032,16 @@ Launch idle throttle - throttle to be set before launch sequence is initiated. I
---
### nav_fw_launch_manual_throttle
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).
| Default | Min | Max |
| --- | --- | --- |
| OFF | OFF | ON |
---
### nav_fw_launch_max_altitude
Altitude (centimeters) at which LAUNCH mode will be turned off and regular flight mode will take over [0-60000].
@ -5052,13 +5082,33 @@ Exposition value used for the PITCH/ROLL axes by all the stabilized flights mode
---
### rc_filter_frequency
### rc_filter_auto
When enabled, INAV will set RC filtering based on refresh rate and smoothing factor.
| Default | Min | Max |
| --- | --- | --- |
| OFF | OFF | ON |
---
### rc_filter_lpf_hz
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
| Default | Min | Max |
| --- | --- | --- |
| 50 | 0 | 100 |
| 50 | 15 | 250 |
---
### rc_filter_smoothing_factor
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
| Default | Min | Max |
| --- | --- | --- |
| 30 | 1 | 100 |
---