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Merge pull request #4078 from dagar/master

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more param metadata cleanup
This commit is contained in:
Lorenz Meier 2016-03-26 12:17:52 +01:00
commit c10b37c2ed
26 changed files with 126 additions and 177 deletions
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2
Tools/px4params/srcparser.py
View File

@ -133,7 +133,7 @@ class SourceParser(object):
re_remove_dots = re.compile(r'\.+$')
re_remove_carriage_return = re.compile('\n+')
valid_tags = set(["group", "board", "min", "max", "unit", "decimal", "increment", "reboot_required", "value"])
valid_tags = set(["group", "board", "min", "max", "unit", "decimal", "increment", "reboot_required", "value", "boolean"])
# Order of parameter groups
priority = {

10
src/drivers/camera_trigger/camera_trigger_params.c
View File

@ -58,7 +58,6 @@ PARAM_DEFINE_FLOAT(TRIG_INTERVAL, 40.0f);
*
* This parameter sets the polarity of the trigger (0 = ACTIVE_LOW, 1 = ACTIVE_HIGH )
*
* @unit enum
* @value 0 ACTIVE_LOW
* @value 1 ACTIVE_HIGH
* @min 0
@ -82,11 +81,10 @@ PARAM_DEFINE_FLOAT(TRIG_ACT_TIME, 0.5f);
*
* 0 disables the trigger, 1 sets it to enabled on command, 2 always on, 3 distance based, 4 distance based enabled on command
*
* @unit enum
* @value 0 disable
* @value 1 cmd
* @value 2 always
* @value 3 distance
* @value 0 Disable
* @value 1 CMD
* @value 2 Always
* @value 3 Distance
* @min 0
* @max 4
* @group Camera trigger

11
src/drivers/gimbal/gimbal_params.c
View File

@ -48,7 +48,7 @@
*
* If set to 1, mount mode will be enforced.
*
* @unit boolean
* @boolean
* @group Gimbal
*/
PARAM_DEFINE_INT32(GMB_USE_MNT, 0);
@ -63,11 +63,10 @@ PARAM_DEFINE_INT32(GMB_USE_MNT, 0);
* Switch on means the gimbal can move freely, and landing gear
* will be retracted if applicable.
*
* @unit enum
* @value 0 disable
* @value 1 aux1
* @value 2 aux2
* @value 3 aux3
* @value 0 Disable
* @value 1 AUX1
* @value 2 AUX2
* @value 3 AUX3
* @min 0
* @max 3
* @group Gimbal

1
src/drivers/mkblctrl/mkblctrl_params.c
View File

@ -46,7 +46,6 @@
/**
* Enables testmode (Identify) of MKBLCTRL Driver
*
* @unit enum
* @value 0 Disabled
* @value 1 Enabled
* @min 0

12
src/drivers/px4fmu/px4fmu_params.c
View File

@ -48,7 +48,7 @@
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_AUX_REV1, 0);
@ -59,7 +59,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV1, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_AUX_REV2, 0);
@ -70,7 +70,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV2, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_AUX_REV3, 0);
@ -81,7 +81,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV3, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_AUX_REV4, 0);
@ -92,7 +92,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV4, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_AUX_REV5, 0);
@ -103,7 +103,7 @@ PARAM_DEFINE_INT32(PWM_AUX_REV5, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_AUX_REV6, 0);

18
src/drivers/px4io/px4io_params.c
View File

@ -48,7 +48,7 @@
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV1, 0);
@ -59,7 +59,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV1, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV2, 0);
@ -70,7 +70,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV2, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV3, 0);
@ -81,7 +81,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV3, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV4, 0);
@ -92,7 +92,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV4, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV5, 0);
@ -103,7 +103,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV5, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV6, 0);
@ -114,7 +114,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV6, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV7, 0);
@ -125,7 +125,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV7, 0);
* Set to 1 to invert the channel, 0 for default direction.
*
* @reboot_required true
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_MAIN_REV8, 0);
@ -135,7 +135,7 @@ PARAM_DEFINE_INT32(PWM_MAIN_REV8, 0);
*
* Set to 1 to enable S.BUS version 1 output instead of RSSI.
*
* @unit boolean
* @boolean
* @group PWM Outputs
*/
PARAM_DEFINE_INT32(PWM_SBUS_MODE, 0);

2
src/lib/launchdetection/launchdetection_params.c
View File

@ -47,7 +47,7 @@
/**
* Enable launch detection.
*
* @unit boolean
* @boolean
* @min 0
* @max 1
* @group Launch detection

7
src/lib/runway_takeoff/runway_takeoff_params.c
View File

@ -44,7 +44,7 @@
*
* 0: disabled, 1: enabled
*
* @unit boolean
* @boolean
* @group Runway Takeoff
*/
PARAM_DEFINE_INT32(RWTO_TKOFF, 0);
@ -54,9 +54,8 @@ PARAM_DEFINE_INT32(RWTO_TKOFF, 0);
*
* 0: airframe heading, 1: heading towards takeoff waypoint
*
* @unit enum
* @value 0 airframe
* @value 1 waypoint
* @value 0 Airframe
* @value 1 Waypoint
* @min 0
* @max 1
* @group Runway Takeoff

11
src/modules/attitude_estimator_q/attitude_estimator_q_params.c
View File

@ -97,7 +97,7 @@ PARAM_DEFINE_FLOAT(ATT_MAG_DECL, 0.0f);
* Enable automatic GPS based declination compensation
*
* @group Attitude Q estimator
* @unit boolean
* @boolean
*/
PARAM_DEFINE_INT32(ATT_MAG_DECL_A, 1);
@ -107,10 +107,9 @@ PARAM_DEFINE_INT32(ATT_MAG_DECL_A, 1);
* Set to 2 to use heading from motion capture.
*
* @group Attitude Q estimator
* @unit enum
* @value 0 none
* @value 1 vision
* @value 2 motion capture
* @value 0 None
* @value 1 Vision
* @value 2 Motion Capture
* @min 0
* @max 2
*/
@ -121,7 +120,7 @@ PARAM_DEFINE_INT32(ATT_EXT_HDG_M, 0);
* velocity.
*
* @group Attitude Q estimator
* @unit boolean
* @boolean
*/
PARAM_DEFINE_INT32(ATT_ACC_COMP, 1);

15
src/modules/commander/commander_params.c
View File

@ -137,7 +137,7 @@ PARAM_DEFINE_FLOAT(BAT_V_LOAD_DROP, 0.07f);
* Defines the number of cells the attached battery consists of.
*
* @group Battery Calibration
* @unit enum
* @unit S
* @min 2
* @max 10
* @value 2 2S Battery
@ -178,7 +178,7 @@ PARAM_DEFINE_FLOAT(BAT_CAPACITY, -1.0f);
* Set to 1 to enable actions triggered when the datalink is lost.
*
* @group Commander
* @unit boolean
* @boolean
*/
PARAM_DEFINE_INT32(COM_DL_LOSS_EN, 0);
@ -303,7 +303,7 @@ PARAM_DEFINE_FLOAT(COM_HOME_V_T, 10.0f);
* being sticky. Developers can default it to off.
*
* @group Commander
* @unit boolean
* @boolean
*/
PARAM_DEFINE_INT32(COM_AUTOS_PAR, 1);
@ -316,7 +316,6 @@ PARAM_DEFINE_INT32(COM_AUTOS_PAR, 1);
* of directly forwarding the manual input data.
*
* @group Commander
* @unit enum
* @min 0
* @max 2
* @value 0 RC Transmitter
@ -347,7 +346,6 @@ PARAM_DEFINE_INT32(COM_DISARM_LAND, 0);
* If the main switch channel is in this range the
* selected flight mode will be applied.
*
* @unit enum
* @value -1 Unassigned
* @value 0 Manual
* @value 1 Altitude
@ -370,7 +368,6 @@ PARAM_DEFINE_INT32(COM_FLTMODE1, -1);
* If the main switch channel is in this range the
* selected flight mode will be applied.
*
* @unit enum
* @value -1 Unassigned
* @value 0 Manual
* @value 1 Altitude
@ -393,7 +390,6 @@ PARAM_DEFINE_INT32(COM_FLTMODE2, -1);
* If the main switch channel is in this range the
* selected flight mode will be applied.
*
* @unit enum
* @value -1 Unassigned
* @value 0 Manual
* @value 1 Altitude
@ -416,7 +412,6 @@ PARAM_DEFINE_INT32(COM_FLTMODE3, -1);
* If the main switch channel is in this range the
* selected flight mode will be applied.
*
* @unit enum
* @value -1 Unassigned
* @value 0 Manual
* @value 1 Altitude
@ -439,7 +434,6 @@ PARAM_DEFINE_INT32(COM_FLTMODE4, -1);
* If the main switch channel is in this range the
* selected flight mode will be applied.
*
* @unit enum
* @value -1 Unassigned
* @value 0 Manual
* @value 1 Altitude
@ -457,12 +451,11 @@ PARAM_DEFINE_INT32(COM_FLTMODE4, -1);
PARAM_DEFINE_INT32(COM_FLTMODE5, -1);
/**
* Sixt flightmode slot (1800-2000)
* Sixth flightmode slot (1800-2000)
*
* If the main switch channel is in this range the
* selected flight mode will be applied.
*
* @unit enum
* @value -1 Unassigned
* @value 0 Manual
* @value 1 Altitude

3
src/modules/ekf2/ekf2_params.c
View File

@ -345,7 +345,6 @@ PARAM_DEFINE_INT32(EKF2_DECL_TYPE, 7);
* If set to automatic: heading fusion on-ground and 3-axis fusion in-flight
*
* @group EKF2
* @unit enum
* @value 0 Automatic
* @value 1 Magnetic heading
* @value 2 3-axis fusion
@ -387,7 +386,7 @@ PARAM_DEFINE_FLOAT(EKF2_GPS_V_GATE, 3.0f);
* replay messages for logging.
*
* @group EKF2
* @unit boolean
* @boolean
*/
PARAM_DEFINE_INT32(EKF2_REC_RPL, 0);

17
src/modules/fw_att_control/fw_att_control_params.c
View File

@ -83,6 +83,7 @@ PARAM_DEFINE_FLOAT(FW_P_TC, 0.4f);
* This defines how much the elevator input will be commanded depending on the
* current body angular rate error.
*
* @unit %/rad/s
* @min 0.005
* @max 1.0
* @group FW Attitude Control
@ -95,6 +96,7 @@ PARAM_DEFINE_FLOAT(FW_PR_P, 0.08f);
* This gain defines how much control response will result out of a steady
* state error. It trims any constant error.
*
* @unit %/rad
* @min 0.005
* @max 0.5
* @group FW Attitude Control
@ -133,6 +135,7 @@ PARAM_DEFINE_FLOAT(FW_P_RMAX_NEG, 60.0f);
* The portion of the integrator part in the control surface deflection is
* limited to this value
*
* @unit %
* @min 0.0
* @max 1.0
* @group FW Attitude Control
@ -145,6 +148,7 @@ PARAM_DEFINE_FLOAT(FW_PR_IMAX, 0.4f);
* This defines how much the aileron input will be commanded depending on the
* current body angular rate error.
*
* @unit %/rad/s
* @min 0.005
* @max 1.0
* @group FW Attitude Control
@ -157,6 +161,7 @@ PARAM_DEFINE_FLOAT(FW_RR_P, 0.05f);
* This gain defines how much control response will result out of a steady
* state error. It trims any constant error.
*
* @unit %/rad
* @min 0.005
* @max 0.2
* @group FW Attitude Control
@ -168,6 +173,7 @@ PARAM_DEFINE_FLOAT(FW_RR_I, 0.01f);
*
* The portion of the integrator part in the control surface deflection is limited to this value.
*
* @unit %
* @min 0.0
* @max 1.0
* @group FW Attitude Control
@ -193,6 +199,7 @@ PARAM_DEFINE_FLOAT(FW_R_RMAX, 70.0f);
* This defines how much the rudder input will be commanded depending on the
* current body angular rate error.
*
* @unit %/rad/s
* @min 0.005
* @max 1.0
* @group FW Attitude Control
@ -205,6 +212,7 @@ PARAM_DEFINE_FLOAT(FW_YR_P, 0.05f);
* This gain defines how much control response will result out of a steady
* state error. It trims any constant error.
*
* @unit %/rad
* @min 0.0
* @max 50.0
* @group FW Attitude Control
@ -217,6 +225,7 @@ PARAM_DEFINE_FLOAT(FW_YR_I, 0.0f);
* The portion of the integrator part in the control surface deflection is
* limited to this value
*
* @unit %
* @min 0.0
* @max 1.0
* @group FW Attitude Control
@ -242,6 +251,7 @@ PARAM_DEFINE_FLOAT(FW_Y_RMAX, 0.0f);
* This defines how much the wheel steering input will be commanded depending on the
* current body angular rate error.
*
* @unit %/rad/s
* @min 0.005
* @max 1.0
* @group FW Attitude Control
@ -254,6 +264,7 @@ PARAM_DEFINE_FLOAT(FW_WR_P, 0.5f);
* This gain defines how much control response will result out of a steady
* state error. It trims any constant error.
*
* @unit %/rad
* @min 0.0
* @max 50.0
* @group FW Attitude Control
@ -266,6 +277,7 @@ PARAM_DEFINE_FLOAT(FW_WR_I, 0.1f);
* The portion of the integrator part in the control surface deflection is
* limited to this value
*
* @unit %
* @min 0.0
* @max 1.0
* @group FW Attitude Control
@ -292,6 +304,7 @@ PARAM_DEFINE_FLOAT(FW_W_RMAX, 0.0f);
* to obtain a tigher response of the controller without introducing
* noise amplification.
*
* @unit %/rad/s
* @min 0.0
* @max 10.0
* @group FW Attitude Control
@ -303,6 +316,7 @@ PARAM_DEFINE_FLOAT(FW_RR_FF, 0.5f);
*
* Direct feed forward from rate setpoint to control surface output
*
* @unit %/rad/s
* @min 0.0
* @max 10.0
* @group FW Attitude Control
@ -314,6 +328,7 @@ PARAM_DEFINE_FLOAT(FW_PR_FF, 0.5f);
*
* Direct feed forward from rate setpoint to control surface output
*
* @unit %/rad/s
* @min 0.0
* @max 10.0
* @group FW Attitude Control
@ -325,6 +340,7 @@ PARAM_DEFINE_FLOAT(FW_YR_FF, 0.3f);
*
* Direct feed forward from rate setpoint to control surface output
*
* @unit %/rad/s
* @min 0.0
* @max 10.0
* @group FW Attitude Control
@ -349,7 +365,6 @@ PARAM_DEFINE_FLOAT(FW_YCO_VMIN, 1000.0f);
* 0: open-loop zero lateral acceleration based on kinematic constraints
* 1: closed-loop: try to reduce lateral acceleration to 0 by measuring the acceleration
*
* @unit enum
* @min 0
* @max 1
* @value 0 open-loop

76
src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c
View File

@ -54,7 +54,7 @@
* @unit m
* @min 12.0
* @max 50.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_L1_PERIOD, 20.0f);
@ -65,7 +65,7 @@ PARAM_DEFINE_FLOAT(FW_L1_PERIOD, 20.0f);
*
* @min 0.6
* @max 0.9
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_L1_DAMPING, 0.75f);
@ -76,7 +76,7 @@ PARAM_DEFINE_FLOAT(FW_L1_DAMPING, 0.75f);
*
* @min 0.0
* @max 1.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_CRUISE, 0.6f);
@ -87,7 +87,7 @@ PARAM_DEFINE_FLOAT(FW_THR_CRUISE, 0.6f);
*
* @min 0.0
* @max 1.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_SLEW_MAX, 0.0f);
@ -99,7 +99,7 @@ PARAM_DEFINE_FLOAT(FW_THR_SLEW_MAX, 0.0f);
* @unit deg
* @min -60.0
* @max 0.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_P_LIM_MIN, -45.0f);
@ -111,7 +111,7 @@ PARAM_DEFINE_FLOAT(FW_P_LIM_MIN, -45.0f);
* @unit deg
* @min 0.0
* @max 60.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_P_LIM_MAX, 45.0f);
@ -123,7 +123,7 @@ PARAM_DEFINE_FLOAT(FW_P_LIM_MAX, 45.0f);
* @unit deg
* @min 35.0
* @max 65.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_R_LIM, 50.0f);
@ -136,7 +136,7 @@ PARAM_DEFINE_FLOAT(FW_R_LIM, 50.0f);
*
* @min 0.0
* @max 1.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_MAX, 1.0f);
@ -154,7 +154,7 @@ PARAM_DEFINE_FLOAT(FW_THR_MAX, 1.0f);
*
* @min 0.0
* @max 1.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
@ -168,7 +168,7 @@ PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
*
* @min 0.0
* @max 0.4
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_IDLE, 0.15f);
@ -180,7 +180,7 @@ PARAM_DEFINE_FLOAT(FW_THR_IDLE, 0.15f);
*
* @min 0.0
* @max 1.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_LND_MAX, 1.0f);
@ -195,7 +195,7 @@ PARAM_DEFINE_FLOAT(FW_THR_LND_MAX, 1.0f);
* @unit m
* @min 0.0
* @max 150.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_CLMBOUT_DIFF, 10.0f);
@ -218,7 +218,7 @@ PARAM_DEFINE_FLOAT(FW_CLMBOUT_DIFF, 10.0f);
* @unit m/s
* @min 2.0
* @max 10.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_CLMB_MAX, 5.0f);
@ -230,7 +230,7 @@ PARAM_DEFINE_FLOAT(FW_T_CLMB_MAX, 5.0f);
* to measure FW_T_CLMB_MAX.
*
* @unit m/s
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_SINK_MIN, 2.0f);
@ -244,7 +244,7 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MIN, 2.0f);
* the aircraft.
*
* @unit m/s
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f);
@ -256,7 +256,7 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f);
* to respond.
*
* @unit s
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_TIME_CONST, 5.0f);
@ -268,7 +268,7 @@ PARAM_DEFINE_FLOAT(FW_T_TIME_CONST, 5.0f);
* to respond.
*
* @unit s
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_THRO_CONST, 8.0f);
@ -278,7 +278,7 @@ PARAM_DEFINE_FLOAT(FW_T_THRO_CONST, 8.0f);
* This is the damping gain for the throttle demand loop.
* Increase to add damping to correct for oscillations in speed and height.
*
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f);
@ -290,7 +290,7 @@ PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f);
* and height offsets are trimmed out, but reduces damping and
* increases overshoot.
*
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f);
@ -304,7 +304,7 @@ PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f);
* from under-speed conditions.
*
* @unit m/s/s
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_VERT_ACC, 7.0f);
@ -318,7 +318,7 @@ PARAM_DEFINE_FLOAT(FW_T_VERT_ACC, 7.0f);
* the solution more towards use of the accelerometer data.
*
* @unit rad/s
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_HGT_OMEGA, 3.0f);
@ -332,7 +332,7 @@ PARAM_DEFINE_FLOAT(FW_T_HGT_OMEGA, 3.0f);
* solution more towards use of the accelerometer data.
*
* @unit rad/s
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_SPD_OMEGA, 2.0f);
@ -348,7 +348,7 @@ PARAM_DEFINE_FLOAT(FW_T_SPD_OMEGA, 2.0f);
* aircraft (eg powered sailplanes) can use a lower value, whereas
* inefficient low aspect-ratio models (eg delta wings) can use a higher value.
*
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_RLL2THR, 15.0f);
@ -368,7 +368,7 @@ PARAM_DEFINE_FLOAT(FW_T_RLL2THR, 15.0f);
*
* @min 0.0
* @max 2.0
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f);
@ -380,28 +380,28 @@ PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f);
* will work well provided the pitch to servo controller has been tuned
* properly.
*
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_PTCH_DAMP, 0.0f);
/**
* Height rate P factor
*
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_HRATE_P, 0.05f);
/**
* Height rate FF factor
*
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.0f);
/**
* Speed rate P factor
*
* @group Fixed Wing TECS
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_SRATE_P, 0.02f);
@ -411,7 +411,7 @@ PARAM_DEFINE_FLOAT(FW_T_SRATE_P, 0.02f);
* @unit deg
* @min 1.0
* @max 15.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_ANG, 5.0f);
@ -419,7 +419,7 @@ PARAM_DEFINE_FLOAT(FW_LND_ANG, 5.0f);
*
*
* @unit m
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_HVIRT, 10.0f);
@ -429,7 +429,7 @@ PARAM_DEFINE_FLOAT(FW_LND_HVIRT, 10.0f);
* @unit m
* @min 0.0
* @max 25.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_FLALT, 8.0f);
@ -442,7 +442,7 @@ PARAM_DEFINE_FLOAT(FW_LND_FLALT, 8.0f);
* @unit m
* @min -1.0
* @max 30.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_TLALT, -1.0f);
@ -452,7 +452,7 @@ PARAM_DEFINE_FLOAT(FW_LND_TLALT, -1.0f);
* @unit m
* @min 0
* @max 30.0
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_HHDIST, 15.0f);
@ -461,8 +461,8 @@ PARAM_DEFINE_FLOAT(FW_LND_HHDIST, 15.0f);
*
* 0: disabled, 1: enabled
*
* @unit boolean
* @group L1 Control
* @boolean
* @group FW L1 Control
*/
PARAM_DEFINE_INT32(FW_LND_USETER, 0);
@ -475,7 +475,7 @@ PARAM_DEFINE_INT32(FW_LND_USETER, 0);
* @unit deg
* @min 0
* @max 15.0
* @group L1 Control
* @group FW L1 Control
*
*/
PARAM_DEFINE_FLOAT(FW_LND_FL_PMIN, 2.5f);
@ -489,7 +489,7 @@ PARAM_DEFINE_FLOAT(FW_LND_FL_PMIN, 2.5f);
* @unit deg
* @min 0
* @max 45.0
* @group L1 Control
* @group FW L1 Control
*
*/
PARAM_DEFINE_FLOAT(FW_LND_FL_PMAX, 15.0f);
@ -502,6 +502,6 @@ PARAM_DEFINE_FLOAT(FW_LND_FL_PMAX, 15.0f);
*
* @min 1.0
* @max 1.5
* @group L1 Control
* @group FW L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_AIRSPD_SC, 1.3f);

2
src/modules/fw_pos_control_l1/mtecs/mTecs_params.c
View File

@ -47,7 +47,7 @@
*
* Set to 1 to enable mTECS
*
* @unit boolean
* @boolean
* @group mTECS
*/
PARAM_DEFINE_INT32(MT_ENABLED, 0);

4
src/modules/local_position_estimator/params.c
View File

@ -6,7 +6,7 @@
/**
* Enable local position estimator.
*
* @unit boolean
* @boolean
* @group Local Position Estimator
*/
PARAM_DEFINE_INT32(LPE_ENABLED, 1);
@ -14,7 +14,7 @@ PARAM_DEFINE_INT32(LPE_ENABLED, 1);
/**
* Enable accelerometer integration for prediction.
*
* @unit boolean
* @boolean
* @group Local Position Estimator
*/
PARAM_DEFINE_INT32(LPE_INTEGRATE, 1);

4
src/modules/mavlink/mavlink_params.c
View File

@ -74,7 +74,7 @@ PARAM_DEFINE_INT32(MAV_TYPE, 1);
*
* If set to 1 incoming HIL GPS messages are parsed.
*
* @unit boolean
* @boolean
* @group MAVLink
*/
PARAM_DEFINE_INT32(MAV_USEHILGPS, 0);
@ -85,7 +85,7 @@ PARAM_DEFINE_INT32(MAV_USEHILGPS, 0);
* If set to 1 incoming external setpoint messages will be directly forwarded
* to the controllers if in offboard control mode
*
* @unit boolean
* @boolean
* @group MAVLink
*/
PARAM_DEFINE_INT32(MAV_FWDEXTSP, 1);

2
src/modules/navigator/datalinkloss_params.c
View File

@ -119,6 +119,6 @@ PARAM_DEFINE_INT32(NAV_DLL_N, 2);
* airfield home
*
* @group Data Link Loss
* @unit boolean
* @boolean
*/
PARAM_DEFINE_INT32(NAV_DLL_CHSK, 0);

13
src/modules/navigator/geofence_params.c
View File

@ -48,14 +48,13 @@
*
* 0 = none, 1 = warning (default), 2 = loiter, 3 = return to launch, 4 = fight termination
*
* @unit enum
* @min 0
* @max 4
* @value 0 none
* @value 1 warning
* @value 2 loiter
* @value 3 return
* @value 4 terminate
* @value 0 None
* @value 1 Warning
* @value 2 Loiter
* @value 3 Return
* @value 4 Terminate
* @group Geofence
*/
PARAM_DEFINE_INT32(GF_ACTION, 1);
@ -66,7 +65,6 @@ PARAM_DEFINE_INT32(GF_ACTION, 1);
* Select which altitude reference should be used
* 0 = WGS84, 1 = AMSL
*
* @unit enum
* @min 0
* @max 1
* @value 0 WGS84
@ -82,7 +80,6 @@ PARAM_DEFINE_INT32(GF_ALTMODE, 0);
* no dependence on the position estimator
* 0 = global position, 1 = GPS
*
* @unit enum
* @min 0
* @max 1
* @value 0 GPOS

19
src/modules/navigator/mission_params.c
View File

@ -73,7 +73,7 @@ PARAM_DEFINE_FLOAT(MIS_LTRMIN_ALT, 1.2f);
* When enabled, missions that have been uploaded by the GCS are stored
* and reloaded after reboot persistently.
*
* @unit boolean
* @boolean
* @group Mission
*/
PARAM_DEFINE_INT32(MIS_ONBOARD_EN, 1);
@ -99,16 +99,10 @@ PARAM_DEFINE_FLOAT(MIS_DIST_1WP, 900);
* 1: the system will follow a first order hold altitude setpoint
* values follow the definition in enum mission_altitude_mode
*
* @unit enum
* @min 0
* @max 1
<<<<<<< e22e0b28b61a7b4f7d10756678b8f4b533b3622e
* @value 0 Zero Order Hold
* @value 1 First Order Hold
=======
* @value 0 zero order
* @value 1 first order
>>>>>>> mission param @unit
* @group Mission
*/
PARAM_DEFINE_INT32(MIS_ALTMODE, 1);
@ -118,20 +112,12 @@ PARAM_DEFINE_INT32(MIS_ALTMODE, 1);
*
* The values are defined in the enum mission_altitude_mode
*
* @unit enum
* @min 0
* @max 3
<<<<<<< e22e0b28b61a7b4f7d10756678b8f4b533b3622e
* @value 0 Heading as set by waypoint
* @value 1 Heading towards waypoint
* @value 2 Heading towards home
* @value 3 Heading away from home
=======
* @value 0 destination
* @value 1 next
* @value 2 home
* @value 3 home back
>>>>>>> mission param @unit
* @group Mission
*/
PARAM_DEFINE_INT32(MIS_YAWMODE, 1);
@ -144,9 +130,9 @@ PARAM_DEFINE_INT32(MIS_YAWMODE, 1);
* Mainly useful for VTOLs that have less yaw authority and might not reach target
* yaw in wind. Disabled by default.
*
* @unit s
* @min -1
* @max 20
* @unit second
* @increment 1
* @group Mission
*/
@ -158,7 +144,6 @@ PARAM_DEFINE_FLOAT(MIS_YAW_TMT, -1.0f);
* @unit deg
* @min 0
* @max 90
* @unit degree
* @increment 1
* @group Mission
*/

4
src/modules/navigator/navigator_params.c
View File

@ -69,7 +69,7 @@ PARAM_DEFINE_FLOAT(NAV_ACC_RAD, 10.0f);
*
* If set to 1 the behaviour on data link loss is set to a mode according to the Outback Challenge (OBC) rules
*
* @unit boolean
* @boolean
* @group Mission
*/
PARAM_DEFINE_INT32(NAV_DLL_OBC, 0);
@ -79,7 +79,7 @@ PARAM_DEFINE_INT32(NAV_DLL_OBC, 0);
*
* If set to 1 the behaviour on data link loss is set to a mode according to the Outback Challenge (OBC) rules
*
* @unit boolean
* @boolean
* @group Mission
*/
PARAM_DEFINE_INT32(NAV_RCL_OBC, 0);

6
src/modules/position_estimator_inav/position_estimator_inav_params.cpp
View File

@ -306,7 +306,7 @@ PARAM_DEFINE_FLOAT(INAV_FLOW_DIST_Y, 0.0f);
*
* Disable mocap
*
* @unit boolean
* @boolean
* @group Position Estimator INAV
*/
PARAM_DEFINE_FLOAT(INAV_DISAB_MOCAP, 0);
@ -316,7 +316,7 @@ PARAM_DEFINE_FLOAT(INAV_DISAB_MOCAP, 0);
*
* Enable LIDAR for altitude estimation
*
* @unit boolean
* @boolean
* @group Position Estimator INAV
*/
PARAM_DEFINE_FLOAT(INAV_LIDAR_EST, 0);
@ -352,7 +352,7 @@ PARAM_DEFINE_INT32(CBRK_NO_VISION, 0);
* Else the system uses the combined attitude / position
* filter framework.
*
* @unit boolean
* @boolean
* @group Position Estimator INAV
*/
PARAM_DEFINE_INT32(INAV_ENABLED, 1);

9
src/modules/sdlog2/params.c
View File

@ -56,12 +56,11 @@ PARAM_DEFINE_INT32(SDLOG_RATE, -1);
* parameter is only read out before logging starts
* (which commonly is before arming).
*
* @unit enum
* @min -1
* @max 1
* @value -1 command line
* @value 0 disable
* @value 1 enable
* @value -1 Command Line
* @value 0 Disable
* @value 1 Enable
* @group SD Logging
*/
PARAM_DEFINE_INT32(SDLOG_EXT, -1);
@ -73,7 +72,7 @@ PARAM_DEFINE_INT32(SDLOG_EXT, -1);
* to only use the time stamp if a 3D GPS lock is
* present.
*
* @unit boolean
* @boolean
* @group SD Logging
*/
PARAM_DEFINE_INT32(SDLOG_GPSTIME, 1);

34
src/modules/sensors/sensor_params.c
View File

@ -329,7 +329,6 @@ PARAM_DEFINE_INT32(CAL_MAG1_ID, 0);
* should only attempt to configure the rotation if the value is
* greater than or equal to zero.
*
* @unit enum
* @value -1 Internal mag
* @value 0 No rotation
* @value 1 Yaw 45°
@ -536,7 +535,6 @@ PARAM_DEFINE_INT32(CAL_MAG2_ID, 0);
* should only attempt to configure the rotation if the value is
* greater than or equal to zero.
*
* @unit enum
* @value -1 Internal mag
* @value 0 No rotation
* @value 1 Yaw 45°
@ -735,7 +733,6 @@ PARAM_DEFINE_FLOAT(SENS_BARO_QNH, 1013.25f);
*
* This parameter defines the rotation of the FMU board relative to the platform.
*
* @unit enum
* @value 0 No rotation
* @value 1 Yaw 45°
* @value 2 Yaw 90°
@ -773,7 +770,6 @@ PARAM_DEFINE_INT32(SENS_BOARD_ROT, 0);
* This parameter defines the rotation of the PX4FLOW board relative to the platform.
* Zero rotation is defined as Y on flow board pointing towards front of vehicle
*
* @unit enum
* @value 0 No rotation
* @value 1 Yaw 45°
* @value 2 Yaw 90°
@ -825,7 +821,6 @@ PARAM_DEFINE_FLOAT(SENS_BOARD_Z_OFF, 0.0f);
/**
* External magnetometer rotation
*
* @unit enum
* @value 0 No rotation
* @value 1 Yaw 45°
* @value 2 Yaw 90°
@ -860,7 +855,6 @@ PARAM_DEFINE_INT32(SENS_EXT_MAG_ROT, 0);
/**
* Select primary magnetometer
*
* @unit enum
* @min 0
* @max 2
* @value 0 Auto-select Mag
@ -1921,7 +1915,6 @@ PARAM_DEFINE_FLOAT(RC18_DZ, 0.0f);
/**
* Enable relay control of relay 1 mapped to the Spektrum receiver power supply
*
* @unit enum
* @min 0
* @max 1
* @value 0 Disabled
@ -1933,7 +1926,6 @@ PARAM_DEFINE_INT32(RC_RL1_DSM_VCC, 0); /* Relay 1 controls DSM VCC */
/**
* DSM binding trigger.
*
* @unit enum
* @value -1 Inactive
* @value 0 Start DSM2 bind
* @value 1 Start DSMX bind
@ -1992,7 +1984,7 @@ PARAM_DEFINE_INT32(RC_CHAN_CNT, 0);
* indicates that the threshold value where automatically set by the ground
* station software. It is only meant for ground station use.
*
* @unit boolean
* @boolean
* @group Radio Calibration
*/
@ -2005,7 +1997,6 @@ PARAM_DEFINE_INT32(RC_TH_USER, 1);
* which channel should be used for reading roll inputs from.
* A value of zero indicates the switch is not assigned.
*
* @unit enum
* @min 0
* @max 18
* @value 0 Unassigned
@ -2038,7 +2029,6 @@ PARAM_DEFINE_INT32(RC_MAP_ROLL, 0);
* which channel should be used for reading pitch inputs from.
* A value of zero indicates the switch is not assigned.
*
* @unit enum
* @min 0
* @max 18
* @value 0 Unassigned
@ -2071,7 +2061,6 @@ PARAM_DEFINE_INT32(RC_MAP_PITCH, 0);
* If 0, whichever channel is mapped to throttle is used
* otherwise the value indicates the specific rc channel to use
*
* @unit enum
* @min 0
* @max 18
* @value 0 Unassigned
@ -2103,7 +2092,6 @@ PARAM_DEFINE_INT32(RC_MAP_FAILSAFE, 0); //Default to throttle function
* which channel should be used for reading throttle inputs from.
* A value of zero indicates the switch is not assigned.
*
* @unit enum
* @min 0
* @max 18
* @value 0 Unassigned
@ -2136,7 +2124,6 @@ PARAM_DEFINE_INT32(RC_MAP_THROTTLE, 0);
* which channel should be used for reading yaw inputs from.
* A value of zero indicates the switch is not assigned.
*
* @unit enum
* @min 0
* @max 18
* @value 0 Unassigned
@ -2168,7 +2155,6 @@ PARAM_DEFINE_INT32(RC_MAP_YAW, 0);
* If this parameter is non-zero, flight modes are only selected
* by this channel and are assigned to six slots.
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2202,7 +2188,6 @@ PARAM_DEFINE_INT32(RC_MAP_FLTMODE, 0);
* which channel should be used for deciding about the main mode.
* A value of zero indicates the switch is not assigned.
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2231,7 +2216,6 @@ PARAM_DEFINE_INT32(RC_MAP_MODE_SW, 0);
/**
* Return switch channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2260,7 +2244,6 @@ PARAM_DEFINE_INT32(RC_MAP_RETURN_SW, 0);
/**
* Rattitude switch channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2289,7 +2272,6 @@ PARAM_DEFINE_INT32(RC_MAP_RATT_SW, 0);
/**
* Position Control switch channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2318,7 +2300,6 @@ PARAM_DEFINE_INT32(RC_MAP_POSCTL_SW, 0);
/**
* Loiter switch channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2347,7 +2328,6 @@ PARAM_DEFINE_INT32(RC_MAP_LOITER_SW, 0);
/**
* Acro switch channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2376,7 +2356,6 @@ PARAM_DEFINE_INT32(RC_MAP_ACRO_SW, 0);
/**
* Offboard switch channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2405,7 +2384,6 @@ PARAM_DEFINE_INT32(RC_MAP_OFFB_SW, 0);
/**
* Kill switch channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2434,7 +2412,6 @@ PARAM_DEFINE_INT32(RC_MAP_KILL_SW, 0);
/**
* Flaps channel
*
* @unit enum
* @min 0
* @max 18
* @group Radio Switches
@ -2465,7 +2442,6 @@ PARAM_DEFINE_INT32(RC_MAP_FLAPS, 0);
*
* Default function: Camera pitch
*
* @unit enum
* @min 0
* @max 18
* @group Radio Calibration
@ -2496,7 +2472,6 @@ PARAM_DEFINE_INT32(RC_MAP_AUX1, 0);
*
* Default function: Camera roll
*
* @unit enum
* @min 0
* @max 18
* @group Radio Calibration
@ -2527,7 +2502,6 @@ PARAM_DEFINE_INT32(RC_MAP_AUX2, 0);
*
* Default function: Camera azimuth / yaw
*
* @unit enum
* @min 0
* @max 18
* @group Radio Calibration
@ -2559,7 +2533,6 @@ PARAM_DEFINE_INT32(RC_MAP_AUX3, 0);
* Can be used for parameter tuning with the RC. This one is further referenced as the 1st parameter channel.
* Set to 0 to deactivate *
*
* @unit enum
* @min 0
* @max 18
* @group Radio Calibration
@ -2591,7 +2564,6 @@ PARAM_DEFINE_INT32(RC_MAP_PARAM1, 0);
* Can be used for parameter tuning with the RC. This one is further referenced as the 2nd parameter channel.
* Set to 0 to deactivate *
*
* @unit enum
* @min 0
* @max 18
* @group Radio Calibration
@ -2623,7 +2595,6 @@ PARAM_DEFINE_INT32(RC_MAP_PARAM2, 0);
* Can be used for parameter tuning with the RC. This one is further referenced as the 3th parameter channel.
* Set to 0 to deactivate *
*
* @unit enum
* @min 0
* @max 18
* @group Radio Calibration
@ -2832,7 +2803,6 @@ PARAM_DEFINE_FLOAT(RC_KILLSWITCH_TH, 0.25f);
*
* Specify the range for RSSI input with RC_RSSI_PWM_MIN and RC_RSSI_PWM_MAX parameters.
*
* @unit enum
* @min 0
* @max 18
* @value 0 Unassigned
@ -2888,7 +2858,7 @@ PARAM_DEFINE_INT32(RC_RSSI_PWM_MIN, 2000);
*
* @reboot_required true
*
* @unit boolean
* @boolean
* @group Sensor Enable
*/
PARAM_DEFINE_INT32(SENS_EN_LL40LS, 0);

1
src/modules/systemlib/system_params.c
View File

@ -90,7 +90,6 @@ PARAM_DEFINE_INT32(SYS_RESTART_TYPE, 2);
* 921600: enables onboard mode at 921600 baud, 8N1. 57600: enables onboard mode at 57600 baud, 8N1.
* 157600: enables OSD mode at 57600 baud, 8N1.
*
* @unit enum
* @value 921600 Companion Link (921600 baud, 8N1)
* @value 57600 Companion Link (57600 baud, 8N1)
* @value 157600 OSD (57600 baud, 8N1)

9
src/modules/uavcan/uavcan_params.c
View File

@ -47,13 +47,12 @@
* 2 - Enabled support for dynamic node ID allocation and firmware update.
* 3 - Sets the motor control outputs to UAVCAN and enables support for dynamic node ID allocation and firmware update.
*
* @unit enum
* @min 0
* @max 3
* @value 0 disabled
* @value 1 enabled
* @value 2 update
* @value 3 motors/update
* @value 0 Disabled
* @value 1 Enabled
* @value 2 Dynamic ID/Update
* @value 3 Motors/Update
* @group UAVCAN
*/
PARAM_DEFINE_INT32(UAVCAN_ENABLE, 0);

11
src/modules/vtol_att_control/vtol_att_control_params.c
View File

@ -110,7 +110,7 @@ PARAM_DEFINE_FLOAT(VT_MC_ARSPD_TRIM, 10.0f);
* If set to one this parameter will cause permanent attitude stabilization in fw mode.
* This parameter has been introduced for pure convenience sake.
*
* @unit boolean
* @boolean
* @group VTOL Attitude Control
*/
PARAM_DEFINE_INT32(VT_FW_PERM_STAB, 0);
@ -172,7 +172,6 @@ PARAM_DEFINE_FLOAT(VT_ARSP_LP_GAIN, 0.3f);
/**
* VTOL Type (Tailsitter=0, Tiltrotor=1, Standard=2)
*
* @unit enum
* @value 0 Tailsitter
* @value 1 Tiltrotor
* @value 2 Standard
@ -188,7 +187,7 @@ PARAM_DEFINE_INT32(VT_TYPE, 0);
*
* If set to 1 the elevons are locked in multicopter mode
*
* @unit boolean
* @boolean
* @group VTOL Attitude Control
*/
PARAM_DEFINE_INT32(VT_ELEV_MC_LOCK, 0);
@ -252,7 +251,7 @@ PARAM_DEFINE_FLOAT(VT_ARSP_TRANS, 10.0f);
/**
* Enable optimal recovery strategy for pitch-weak tailsitters
*
* @unit boolean
* @boolean
* @group VTOL Attitude Control
*/
PARAM_DEFINE_INT32(VT_OPT_RECOV_EN, 0);
@ -260,7 +259,7 @@ PARAM_DEFINE_INT32(VT_OPT_RECOV_EN, 0);
/**
* Enable weather-vane mode landings for missions
*
* @unit boolean
* @boolean
* @group VTOL Attitude Control
*/
PARAM_DEFINE_INT32(VT_WV_LND_EN, 0);
@ -282,7 +281,7 @@ PARAM_DEFINE_FLOAT(VT_WV_YAWR_SCL, 0.15f);
/**
* Enable weather-vane mode for loiter
*
* @unit boolean
* @boolean
* @group VTOL Attitude Control
*/
PARAM_DEFINE_INT32(VT_WV_LTR_EN, 0);