diff --git a/docs/Cli.md b/docs/Cli.md index 7d9013844..95fa09f76 100644 --- a/docs/Cli.md +++ b/docs/Cli.md @@ -251,11 +251,15 @@ Re-apply any new defaults as desired. | `yaw_p_limit` | Limiter for yaw P term. This parameter is only affecting PID controller MW23. To disable set to 500 (actual default). | 100 | 500 | 500 | Profile | UINT16 | | `blackbox_rate_num` | | 1 | 32 | 1 | Master | UINT8 | | `blackbox_rate_denom` | | 1 | 32 | 1 | Master | UINT8 | -| `mag_hold_rate_limit` | This setting limits yaw rotation rate that MAG_HOLD controller can request from PID inner loop controller. It is independent from manual yaw rate and used only when MAG_HOLD flight mode is enabled by pilot, RTH or WAYPOINT modes.| 10 | 255 | 40 | Profile | UINT8 | -| `nav_max_climb_rate` | Maximum climb/descent rate that UAV is allowed to reach during navigation modes. In cm/s | 10 | 2000 | 500 | Master | UINT16 | -| `flaperon_throw_offset` | Defines throw range in us for both ailerons that will be applied (before scaling) when FLAPERON mode is activated. | 100 | 400 | 250 | Profile | UINT16 | -| `flaperon_throw_inverted` | Inverts throw offset on both ailerons. Can be used to create SPOILERON or just to change throw direction | OFF | ON | OFF | Profile | UINT8 | -| `fw_iterm_throw_limit` | 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. | 0 | 500 | 165 | Profile | UINT16 | +| `mag_hold_rate_limit` | This setting limits yaw rotation rate that MAG_HOLD controller can request from PID inner loop controller. It is independent from manual yaw rate and used only when MAG_HOLD flight mode is enabled by pilot, RTH or WAYPOINT modes.| 10 | 255 | 40 | Profile | UINT8 | +| `nav_max_climb_rate` | Maximum climb/descent rate that UAV is allowed to reach during navigation modes. In cm/s | 10 | 2000 | 500 | Master | UINT16 | +| `flaperon_throw_offset` | Defines throw range in us for both ailerons that will be applied (before scaling) when FLAPERON mode is activated. | 100 | 400 | 250 | Profile | UINT16 | +| `flaperon_throw_inverted` | Inverts throw offset on both ailerons. Can be used to create SPOILERON or just to change throw direction | OFF | ON | OFF | Profile | UINT8 | +| `fw_iterm_throw_limit` | 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. | 0 | 500 | 165 | Profile | UINT16 | +| `iterm_ignore_threshold` | Used to prevent Iterm accumulation on ROLL/PITCH axis during stick movements. Iterm is allowed to change fully when sticks are centered. Iterm will not change when requested rotation speed is above `iterm_ignore_threshold`. Iterm acumulation is scaled lineary between `0` and `iterm_ignore_threshold` | 15 | 1000 | 200 | Profile | UINT8 | +| `yaw_iterm_ignore_threshold` | Used to prevent Iterm accumulation on YAW axis during stick movements. Iterm is allowed to change fully when sticks are centered. Iterm will not change when requested rotation speed is above `yaw_iterm_ignore_threshold`. Iterm acumulation is scaled lineary between `0` and `yaw_iterm_ignore_threshold` | 15 | 1000 | 50 | Profile | UINT8 | +| `rate_accel_limit_roll_pitch` | 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. Disabled by default. | 0 | 500000 | 0 | Profile | UINT8 | +| `rate_accel_limit_yaw` | 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 durig yaw turns. Value of `0` disables limiting. Enabled by default. | 0 | 500000 | 10000 | Profile | UINT8 | ## New iNav specific | `Variable` | Description/Units | Min | Max | Default | Type | Datatype |