mirror of https://github.com/ArduPilot/ardupilot
Plane: Default Q_FWD_THR_GAIN to 0 and update meta data
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@ -507,11 +507,11 @@ const AP_Param::GroupInfo QuadPlane::var_info2[] = {
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// @Param: FWD_THR_GAIN
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// @DisplayName: Q mode fwd throttle gain
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// @Description: Gain from forward accel/tilt to forward throttle that is used in all VTOL modes except autotune. Vehicles using separate forward thrust motors, eg quadplanes, should set this parameter to (all up weight) / (maximum combined thrust of forward motors). Vehicles that tilt lifting rotors to provide forward thrust should set this parameter to (all up weight) / (weight lifted by tilting rotors) which for most aircraft can be approximnated as (total number of lifting rotors) / (number of lifting rotors that tilt). When using this method of forward throttle control, the forward tilt angle limit is controlled by the Q_FWD_PIT_LIM parameter and the Q_VFWD_GAIN parameter should be set to 0 to disable the alternative method that works through the velocity controller. Set Q_FWD_THR_GAIN to 0 to disable this function. Do not use this parameter with tail sitters.
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// @Description: Gain from forward accel/tilt to forward throttle that is used in all VTOL modes except autotune. Vehicles using separate forward thrust motors, eg quadplanes, should set this parameter to (all up weight) / (maximum combined thrust of forward motors) with a value of 2 being typical. Vehicles that tilt lifting rotors to provide forward thrust should set this parameter to (all up weight) / (weight lifted by tilting rotors) which for most aircraft can be approximated as (total number of lifting rotors) / (number of lifting rotors that tilt). When using this method of forward throttle control, the forward tilt angle limit is controlled by the Q_FWD_PIT_LIM parameter and the Q_VFWD_GAIN parameter should be set to 0 to disable the alternative method that works through the velocity controller. Set Q_FWD_THR_GAIN to 0 to disable this function. Do not use this parameter with tail sitters.
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// @Range: 0.0 5.0
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// @Increment: 0.1
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// @User: Standard
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AP_GROUPINFO("FWD_THR_GAIN", 35, QuadPlane, q_fwd_thr_gain, 2.0f),
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AP_GROUPINFO("FWD_THR_GAIN", 35, QuadPlane, q_fwd_thr_gain, 0.0f),
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// @Param: FWD_PIT_LIM
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// @DisplayName: Q mode forward pitch limit
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