forked from Archive/PX4-Autopilot
runway_takeoff_params.c param metadata
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@ -42,8 +42,6 @@
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/**
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/**
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* Enable or disable runway takeoff with landing gear
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* Enable or disable runway takeoff with landing gear
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*
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*
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* 0: disabled, 1: enabled
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*
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* @boolean
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* @boolean
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* @group Runway Takeoff
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* @group Runway Takeoff
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*/
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*/
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@ -71,6 +69,8 @@ PARAM_DEFINE_INT32(RWTO_HDG, 0);
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* @unit m
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* @unit m
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* @min 0.0
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* @min 0.0
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* @max 100.0
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* @max 100.0
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* @decimal 1
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* @increment 1
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* @group Runway Takeoff
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* @group Runway Takeoff
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*/
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*/
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PARAM_DEFINE_FLOAT(RWTO_NAV_ALT, 5.0);
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PARAM_DEFINE_FLOAT(RWTO_NAV_ALT, 5.0);
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@ -79,8 +79,11 @@ PARAM_DEFINE_FLOAT(RWTO_NAV_ALT, 5.0);
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* Max throttle during runway takeoff.
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* Max throttle during runway takeoff.
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* (Can be used to test taxi on runway)
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* (Can be used to test taxi on runway)
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*
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*
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* @unit norm
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* @min 0.0
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* @min 0.0
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* @max 1.0
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* @max 1.0
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* @decimal 2
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* @increment 0.01
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* @group Runway Takeoff
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* @group Runway Takeoff
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*/
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*/
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PARAM_DEFINE_FLOAT(RWTO_MAX_THR, 1.0);
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PARAM_DEFINE_FLOAT(RWTO_MAX_THR, 1.0);
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@ -94,6 +97,8 @@ PARAM_DEFINE_FLOAT(RWTO_MAX_THR, 1.0);
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* @unit deg
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* @unit deg
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* @min 0.0
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* @min 0.0
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* @max 20.0
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* @max 20.0
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* @decimal 1
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* @increment 0.5
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* @group Runway Takeoff
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* @group Runway Takeoff
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*/
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*/
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PARAM_DEFINE_FLOAT(RWTO_PSP, 0.0);
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PARAM_DEFINE_FLOAT(RWTO_PSP, 0.0);
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@ -106,6 +111,8 @@ PARAM_DEFINE_FLOAT(RWTO_PSP, 0.0);
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* @unit deg
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* @unit deg
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* @min 0.0
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* @min 0.0
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* @max 60.0
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* @max 60.0
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* @decimal 1
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* @increment 0.5
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* @group Runway Takeoff
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* @group Runway Takeoff
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*/
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*/
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PARAM_DEFINE_FLOAT(RWTO_MAX_PITCH, 20.0);
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PARAM_DEFINE_FLOAT(RWTO_MAX_PITCH, 20.0);
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@ -118,6 +125,8 @@ PARAM_DEFINE_FLOAT(RWTO_MAX_PITCH, 20.0);
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* @unit deg
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* @unit deg
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* @min 0.0
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* @min 0.0
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* @max 60.0
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* @max 60.0
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* @decimal 1
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* @increment 0.5
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* @group Runway Takeoff
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* @group Runway Takeoff
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*/
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*/
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PARAM_DEFINE_FLOAT(RWTO_MAX_ROLL, 25.0);
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PARAM_DEFINE_FLOAT(RWTO_MAX_ROLL, 25.0);
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@ -127,8 +136,11 @@ PARAM_DEFINE_FLOAT(RWTO_MAX_ROLL, 25.0);
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* Pitch up will be commanded when the following airspeed is reached:
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* Pitch up will be commanded when the following airspeed is reached:
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* FW_AIRSPD_MIN * RWTO_AIRSPD_SCL
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* FW_AIRSPD_MIN * RWTO_AIRSPD_SCL
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*
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*
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* @unit norm
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* @min 0.0
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* @min 0.0
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* @max 2.0
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* @max 2.0
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* @decimal 2
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* @increment 0.01
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* @group Runway Takeoff
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* @group Runway Takeoff
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*/
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*/
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PARAM_DEFINE_FLOAT(RWTO_AIRSPD_SCL, 1.3);
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PARAM_DEFINE_FLOAT(RWTO_AIRSPD_SCL, 1.3);
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