<long_desc>Scale factor applied to the desired pitch actuator command in full manual mode. This parameter allows to adjust the throws of the control surfaces.</long_desc>
<long_desc>Scale factor applied to the desired roll actuator command in full manual mode. This parameter allows to adjust the throws of the control surfaces.</long_desc>
<long_desc>This is the maximally added yaw rate setpoint from the yaw stick in any attitude controlled flight mode. The controller already generates a yaw rate setpoint to coordinate a turn, and this value is added to it. This is an absolute value, which is applied symmetrically to the negative and positive side.</long_desc>
<long_desc>Scale factor applied to the desired yaw actuator command in full manual mode. This parameter allows to adjust the throws of the control surfaces.</long_desc>
<short_desc>Pitch setpoint offset (pitch at level flight)</short_desc>
<long_desc>An airframe specific offset of the pitch setpoint in degrees, the value is added to the pitch setpoint and should correspond to the pitch at typical cruise speed of the airframe.</long_desc>
<short_desc>Roll control to yaw control feedforward gain</short_desc>
<long_desc>This gain can be used to counteract the "adverse yaw" effect for fixed wings. When the plane enters a roll it will tend to yaw the nose out of the turn. This gain enables the use of a yaw actuator to counteract this effect.</long_desc>
<long_desc>This enables a logic that automatically adjusts the output of the rate controller to take into account the real torque produced by an aerodynamic control surface given the current deviation from the trim airspeed (FW_AIRSPD_TRIM). Enable when using aerodynamic control surfaces (e.g.: plane) Disable when using rotor wings (e.g.: autogyro)</long_desc>
<long_desc>Scale factor applied to the desired pitch actuator command in full manual mode. This parameter allows to adjust the throws of the control surfaces.</long_desc>
<long_desc>Scale factor applied to the desired roll actuator command in full manual mode. This parameter allows to adjust the throws of the control surfaces.</long_desc>
<long_desc>Scale factor applied to the desired yaw actuator command in full manual mode. This parameter allows to adjust the throws of the control surfaces.</long_desc>
<short_desc>Roll control to yaw control feedforward gain</short_desc>
<long_desc>This gain can be used to counteract the "adverse yaw" effect for fixed wings. When the plane enters a roll it will tend to yaw the nose out of the turn. This gain enables the use of a yaw actuator to counteract this effect.</long_desc>
<long_desc>The maximal airspeed (calibrated airspeed) the user is able to command.</long_desc>
<min>0.5</min>
<max>40</max>
<unit>m/s</unit>
<decimal>1</decimal>
<increment>0.5</increment>
@ -3221,7 +3220,6 @@
@@ -3221,7 +3220,6 @@
<short_desc>Minimum Airspeed (CAS)</short_desc>
<long_desc>The minimal airspeed (calibrated airspeed) the user is able to command. Further, if the airspeed falls below this value, the TECS controller will try to increase airspeed more aggressively. Has to be set according to the vehicle's stall speed (which should be set in FW_AIRSPD_STALL), with some margin between the stall speed and minimum airspeed. This value corresponds to the desired minimum speed with the default load factor (level flight, default weight), and is automatically adpated to the current load factor (calculated from roll setpoint and WEIGHT_GROSS/WEIGHT_BASE).</long_desc>
<min>0.5</min>
<max>40</max>
<unit>m/s</unit>
<decimal>1</decimal>
<increment>0.5</increment>
@ -3230,7 +3228,6 @@
@@ -3230,7 +3228,6 @@
<short_desc>Stall Airspeed (CAS)</short_desc>
<long_desc>The stall airspeed (calibrated airspeed) of the vehicle. It is used for airspeed sensor failure detection and for the control surface scaling airspeed limits.</long_desc>
<min>0.5</min>
<max>40</max>
<unit>m/s</unit>
<decimal>1</decimal>
<increment>0.5</increment>
@ -3239,7 +3236,6 @@
@@ -3239,7 +3236,6 @@
<short_desc>Trim (Cruise) Airspeed</short_desc>
<long_desc>The trim CAS (calibrated airspeed) of the vehicle. If an airspeed controller is active, this is the default airspeed setpoint that the controller will try to achieve.</long_desc>
<long_desc>This is the integrator gain on the throttle part of the control loop. Increasing this gain increases the speed at which speed and height offsets are trimmed out, but reduces damping and increases overshoot. Set this value to zero to completely disable all integrator action.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
PX4BuildBot
2 years ago