forked from Archive/PX4-Autopilot
params correct boolean tag
This commit is contained in:
parent
ff9b8118ab
commit
70a68def83
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@ -48,7 +48,7 @@
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*
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* If set to 1, mount mode will be enforced.
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*
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* @unit boolean
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* @boolean
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* @group Gimbal
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*/
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PARAM_DEFINE_INT32(GMB_USE_MNT, 0);
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@ -48,7 +48,7 @@
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_AUX_REV1, 0);
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@ -59,7 +59,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV1, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_AUX_REV2, 0);
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@ -70,7 +70,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV2, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_AUX_REV3, 0);
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@ -81,7 +81,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV3, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_AUX_REV4, 0);
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@ -92,7 +92,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV4, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_AUX_REV5, 0);
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@ -103,7 +103,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV5, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_AUX_REV6, 0);
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@ -48,7 +48,7 @@
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV1, 0);
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@ -59,7 +59,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV1, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV2, 0);
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@ -70,7 +70,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV2, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV3, 0);
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@ -81,7 +81,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV3, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV4, 0);
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@ -92,7 +92,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV4, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV5, 0);
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@ -103,7 +103,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV5, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV6, 0);
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@ -114,7 +114,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV6, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV7, 0);
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@ -125,7 +125,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV7, 0);
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* Set to 1 to invert the channel, 0 for default direction.
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*
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* @reboot_required true
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_MAIN_REV8, 0);
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@ -135,7 +135,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV8, 0);
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*
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* Set to 1 to enable S.BUS version 1 output instead of RSSI.
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*
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* @unit boolean
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* @boolean
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* @group PWM Outputs
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*/
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PARAM_DEFINE_INT32(PWM_SBUS_MODE, 0);
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@ -47,7 +47,7 @@
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/**
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* Enable launch detection.
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*
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* @unit boolean
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* @boolean
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* @min 0
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* @max 1
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* @group Launch detection
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@ -44,7 +44,7 @@
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*
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* 0: disabled, 1: enabled
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*
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* @unit boolean
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* @boolean
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* @group Runway Takeoff
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*/
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PARAM_DEFINE_INT32(RWTO_TKOFF, 0);
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@ -97,7 +97,7 @@ PARAM_DEFINE_FLOAT(ATT_MAG_DECL, 0.0f);
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* Enable automatic GPS based declination compensation
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*
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* @group Attitude Q estimator
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* @unit boolean
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* @boolean
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*/
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PARAM_DEFINE_INT32(ATT_MAG_DECL_A, 1);
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@ -121,7 +121,7 @@ PARAM_DEFINE_INT32(ATT_EXT_HDG_M, 0);
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* velocity.
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*
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* @group Attitude Q estimator
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* @unit boolean
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* @boolean
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*/
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PARAM_DEFINE_INT32(ATT_ACC_COMP, 1);
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@ -178,7 +178,7 @@ PARAM_DEFINE_FLOAT(BAT_CAPACITY, -1.0f);
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* Set to 1 to enable actions triggered when the datalink is lost.
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*
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* @group Commander
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* @unit boolean
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* @boolean
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*/
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PARAM_DEFINE_INT32(COM_DL_LOSS_EN, 0);
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@ -303,7 +303,7 @@ PARAM_DEFINE_FLOAT(COM_HOME_V_T, 10.0f);
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* being sticky. Developers can default it to off.
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*
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* @group Commander
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* @unit boolean
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* @boolean
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*/
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PARAM_DEFINE_INT32(COM_AUTOS_PAR, 1);
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@ -387,7 +387,7 @@ PARAM_DEFINE_FLOAT(EKF2_GPS_V_GATE, 3.0f);
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* replay messages for logging.
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*
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* @group EKF2
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* @unit boolean
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* @boolean
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*/
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PARAM_DEFINE_INT32(EKF2_REC_RPL, 0);
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@ -461,7 +461,7 @@ PARAM_DEFINE_FLOAT(FW_LND_HHDIST, 15.0f);
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*
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* 0: disabled, 1: enabled
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*
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* @unit boolean
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* @boolean
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* @group FW L1 Control
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*/
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PARAM_DEFINE_INT32(FW_LND_USETER, 0);
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@ -47,7 +47,7 @@
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*
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* Set to 1 to enable mTECS
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*
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* @unit boolean
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* @boolean
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* @group mTECS
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*/
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PARAM_DEFINE_INT32(MT_ENABLED, 0);
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@ -6,7 +6,7 @@
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/**
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* Enable local position estimator.
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*
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* @unit boolean
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* @boolean
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* @group Local Position Estimator
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*/
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PARAM_DEFINE_INT32(LPE_ENABLED, 1);
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@ -14,7 +14,7 @@ PARAM_DEFINE_INT32(LPE_ENABLED, 1);
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/**
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* Enable accelerometer integration for prediction.
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*
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* @unit boolean
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* @boolean
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* @group Local Position Estimator
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*/
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PARAM_DEFINE_INT32(LPE_INTEGRATE, 1);
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@ -74,7 +74,7 @@ PARAM_DEFINE_INT32(MAV_TYPE, 1);
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*
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* If set to 1 incoming HIL GPS messages are parsed.
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*
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* @unit boolean
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* @boolean
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* @group MAVLink
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*/
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PARAM_DEFINE_INT32(MAV_USEHILGPS, 0);
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@ -85,7 +85,7 @@ PARAM_DEFINE_INT32(MAV_USEHILGPS, 0);
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* If set to 1 incoming external setpoint messages will be directly forwarded
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* to the controllers if in offboard control mode
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*
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* @unit boolean
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* @boolean
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* @group MAVLink
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*/
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PARAM_DEFINE_INT32(MAV_FWDEXTSP, 1);
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@ -119,6 +119,6 @@ PARAM_DEFINE_INT32(NAV_DLL_N, 2);
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* airfield home
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*
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* @group Data Link Loss
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* @unit boolean
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* @boolean
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*/
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PARAM_DEFINE_INT32(NAV_DLL_CHSK, 0);
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@ -73,7 +73,7 @@ PARAM_DEFINE_FLOAT(MIS_LTRMIN_ALT, 1.2f);
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* When enabled, missions that have been uploaded by the GCS are stored
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* and reloaded after reboot persistently.
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*
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* @unit boolean
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* @boolean
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* @group Mission
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*/
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PARAM_DEFINE_INT32(MIS_ONBOARD_EN, 1);
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@ -69,7 +69,7 @@ PARAM_DEFINE_FLOAT(NAV_ACC_RAD, 10.0f);
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*
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* If set to 1 the behaviour on data link loss is set to a mode according to the Outback Challenge (OBC) rules
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*
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* @unit boolean
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* @boolean
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* @group Mission
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*/
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PARAM_DEFINE_INT32(NAV_DLL_OBC, 0);
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@ -79,7 +79,7 @@ PARAM_DEFINE_INT32(NAV_DLL_OBC, 0);
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*
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* If set to 1 the behaviour on data link loss is set to a mode according to the Outback Challenge (OBC) rules
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*
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* @unit boolean
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* @boolean
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* @group Mission
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*/
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PARAM_DEFINE_INT32(NAV_RCL_OBC, 0);
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@ -306,7 +306,7 @@ PARAM_DEFINE_FLOAT(INAV_FLOW_DIST_Y, 0.0f);
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*
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* Disable mocap
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*
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* @unit boolean
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* @boolean
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* @group Position Estimator INAV
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*/
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PARAM_DEFINE_FLOAT(INAV_DISAB_MOCAP, 0);
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@ -316,7 +316,7 @@ PARAM_DEFINE_FLOAT(INAV_DISAB_MOCAP, 0);
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*
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* Enable LIDAR for altitude estimation
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*
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* @unit boolean
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* @boolean
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* @group Position Estimator INAV
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*/
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PARAM_DEFINE_FLOAT(INAV_LIDAR_EST, 0);
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@ -352,7 +352,7 @@ PARAM_DEFINE_INT32(CBRK_NO_VISION, 0);
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* Else the system uses the combined attitude / position
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* filter framework.
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*
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* @unit boolean
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* @boolean
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* @group Position Estimator INAV
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*/
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PARAM_DEFINE_INT32(INAV_ENABLED, 1);
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@ -73,7 +73,7 @@ PARAM_DEFINE_INT32(SDLOG_EXT, -1);
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* to only use the time stamp if a 3D GPS lock is
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* present.
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*
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* @unit boolean
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* @boolean
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* @group SD Logging
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*/
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PARAM_DEFINE_INT32(SDLOG_GPSTIME, 1);
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@ -1992,7 +1992,7 @@ PARAM_DEFINE_INT32(RC_CHAN_CNT, 0);
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* indicates that the threshold value where automatically set by the ground
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* station software. It is only meant for ground station use.
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*
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* @unit boolean
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* @boolean
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* @group Radio Calibration
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*/
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@ -2888,7 +2888,7 @@ PARAM_DEFINE_INT32(RC_RSSI_PWM_MIN, 2000);
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*
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* @reboot_required true
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*
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* @unit boolean
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* @boolean
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* @group Sensor Enable
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*/
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PARAM_DEFINE_INT32(SENS_EN_LL40LS, 0);
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@ -110,7 +110,7 @@ PARAM_DEFINE_FLOAT(VT_MC_ARSPD_TRIM, 10.0f);
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* If set to one this parameter will cause permanent attitude stabilization in fw mode.
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* This parameter has been introduced for pure convenience sake.
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*
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* @unit boolean
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* @boolean
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* @group VTOL Attitude Control
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*/
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PARAM_DEFINE_INT32(VT_FW_PERM_STAB, 0);
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@ -188,7 +188,7 @@ PARAM_DEFINE_INT32(VT_TYPE, 0);
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*
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* If set to 1 the elevons are locked in multicopter mode
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*
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* @unit boolean
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* @boolean
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* @group VTOL Attitude Control
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*/
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PARAM_DEFINE_INT32(VT_ELEV_MC_LOCK, 0);
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@ -252,7 +252,7 @@ PARAM_DEFINE_FLOAT(VT_ARSP_TRANS, 10.0f);
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/**
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* Enable optimal recovery strategy for pitch-weak tailsitters
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*
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* @unit boolean
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* @boolean
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* @group VTOL Attitude Control
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*/
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PARAM_DEFINE_INT32(VT_OPT_RECOV_EN, 0);
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@ -260,7 +260,7 @@ PARAM_DEFINE_INT32(VT_OPT_RECOV_EN, 0);
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/**
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* Enable weather-vane mode landings for missions
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*
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* @unit boolean
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* @boolean
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* @group VTOL Attitude Control
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*/
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PARAM_DEFINE_INT32(VT_WV_LND_EN, 0);
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@ -282,7 +282,7 @@ PARAM_DEFINE_FLOAT(VT_WV_YAWR_SCL, 0.15f);
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/**
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* Enable weather-vane mode for loiter
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*
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* @unit boolean
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* @boolean
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* @group VTOL Attitude Control
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*/
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PARAM_DEFINE_INT32(VT_WV_LTR_EN, 0);
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