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Merge remote-tracking branch 'px4/beta' into beta_mavlink

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This commit is contained in:
Julian Oes
2014-02-16 12:37:15 +01:00
parent 12d8a7109c ab2f260f77
commit 875ba3bb2b
19 changed files with 802 additions and 195 deletions
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src/modules/commander/commander_params.c
+32
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@@ -48,7 +48,39 @@
PARAM_DEFINE_FLOAT(TRIM_ROLL, 0.0f);
PARAM_DEFINE_FLOAT(TRIM_PITCH, 0.0f);
PARAM_DEFINE_FLOAT(TRIM_YAW, 0.0f);
/**
* Empty cell voltage.
*
* Defines the voltage where a single cell of the battery is considered empty.
*
* @group Battery Calibration
*/
PARAM_DEFINE_FLOAT(BAT_V_EMPTY, 3.4f);
/**
* Full cell voltage.
*
* Defines the voltage where a single cell of the battery is considered full.
*
* @group Battery Calibration
*/
PARAM_DEFINE_FLOAT(BAT_V_FULL, 3.9f);
/**
* Number of cells.
*
* Defines the number of cells the attached battery consists of.
*
* @group Battery Calibration
*/
PARAM_DEFINE_INT32(BAT_N_CELLS, 3);
/**
* Battery capacity.
*
* Defines the capacity of the attached battery.
*
* @group Battery Calibration
*/
PARAM_DEFINE_FLOAT(BAT_CAPACITY, -1.0f);
src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c
+244 -36
View File
@@ -40,12 +40,10 @@
*/
#include <nuttx/config.h>
#include <systemlib/param/param.h>
/*
* Controller parameters, accessible via MAVLink
*
*/
/**
@@ -119,58 +117,268 @@ PARAM_DEFINE_FLOAT(FW_P_LIM_MIN, -45.0f);
*/
PARAM_DEFINE_FLOAT(FW_P_LIM_MAX, 45.0f);
/**
* Controller roll limit
*
* The maximum roll the controller will output.
*
* @unit degrees
* @min 0.0
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_R_LIM, 45.0f);
PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
/**
* Throttle limit max
*
* This is the maximum throttle % that can be used by the controller.
* For overpowered aircraft, this should be reduced to a value that
* provides sufficient thrust to climb at the maximum pitch angle PTCH_MAX.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_MAX, 1.0f);
/**
* Throttle limit min
*
* This is the minimum throttle % that can be used by the controller.
* For electric aircraft this will normally be set to zero, but can be set
* to a small non-zero value if a folding prop is fitted to prevent the
* prop from folding and unfolding repeatedly in-flight or to provide
* some aerodynamic drag from a turning prop to improve the descent rate.
*
* For aircraft with internal combustion engine this parameter should be set
* for desired idle rpm.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
/**
* Throttle limit value before flare
*
* This throttle value will be set as throttle limit at FW_LND_TLALT,
* before arcraft will flare.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_THR_LND_MAX, 1.0f);
/**
* Maximum climb rate
*
* This is the best climb rate that the aircraft can achieve with
* the throttle set to THR_MAX and the airspeed set to the
* default value. For electric aircraft make sure this number can be
* achieved towards the end of flight when the battery voltage has reduced.
* The setting of this parameter can be checked by commanding a positive
* altitude change of 100m in loiter, RTL or guided mode. If the throttle
* required to climb is close to THR_MAX and the aircraft is maintaining
* airspeed, then this parameter is set correctly. If the airspeed starts
* to reduce, then the parameter is set to high, and if the throttle
* demand required to climb and maintain speed is noticeably less than
* FW_THR_MAX, then either FW_T_CLMB_MAX should be increased or
* FW_THR_MAX reduced.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_CLMB_MAX, 5.0f);
/**
* Minimum descent rate
*
* This is the sink rate of the aircraft with the throttle
* set to THR_MIN and flown at the same airspeed as used
* to measure FW_T_CLMB_MAX.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_SINK_MIN, 2.0f);
PARAM_DEFINE_FLOAT(FW_T_TIME_CONST, 5.0f);
PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f);
PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f);
PARAM_DEFINE_FLOAT(FW_T_VERT_ACC, 7.0f);
PARAM_DEFINE_FLOAT(FW_T_HGT_OMEGA, 3.0f);
PARAM_DEFINE_FLOAT(FW_T_SPD_OMEGA, 2.0f);
PARAM_DEFINE_FLOAT(FW_T_RLL2THR, 10.0f);
PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f);
PARAM_DEFINE_FLOAT(FW_T_PTCH_DAMP, 0.0f);
/**
* Maximum descent rate
*
* This sets the maximum descent rate that the controller will use.
* If this value is too large, the aircraft can over-speed on descent.
* This should be set to a value that can be achieved without
* exceeding the lower pitch angle limit and without over-speeding
* the aircraft.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f);
/**
* TECS time constant
*
* This is the time constant of the TECS control algorithm (in seconds).
* Smaller values make it faster to respond, larger values make it slower
* to respond.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_TIME_CONST, 5.0f);
/**
* Throttle damping factor
*
* This is the damping gain for the throttle demand loop.
* Increase to add damping to correct for oscillations in speed and height.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f);
/**
* Integrator gain
*
* This is the integrator gain on the control loop.
* Increasing this gain increases the speed at which speed
* and height offsets are trimmed out, but reduces damping and
* increases overshoot.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f);
/**
* Maximum vertical acceleration
*
* This is the maximum vertical acceleration (in metres/second^2)
* either up or down that the controller will use to correct speed
* or height errors. The default value of 7 m/s/s (equivalent to +- 0.7 g)
* allows for reasonably aggressive pitch changes if required to recover
* from under-speed conditions.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_VERT_ACC, 7.0f);
/**
* Complementary filter "omega" parameter for height
*
* This is the cross-over frequency (in radians/second) of the complementary
* filter used to fuse vertical acceleration and barometric height to obtain
* an estimate of height rate and height. Increasing this frequency weights
* the solution more towards use of the barometer, whilst reducing it weights
* the solution more towards use of the accelerometer data.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_HGT_OMEGA, 3.0f);
/**
* Complementary filter "omega" parameter for speed
*
* This is the cross-over frequency (in radians/second) of the complementary
* filter used to fuse longitudinal acceleration and airspeed to obtain an
* improved airspeed estimate. Increasing this frequency weights the solution
* more towards use of the arispeed sensor, whilst reducing it weights the
* solution more towards use of the accelerometer data.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_SPD_OMEGA, 2.0f);
/**
* Roll -> Throttle feedforward
*
* Increasing this gain turn increases the amount of throttle that will
* be used to compensate for the additional drag created by turning.
* Ideally this should be set to approximately 10 x the extra sink rate
* in m/s created by a 45 degree bank turn. Increase this gain if
* the aircraft initially loses energy in turns and reduce if the
* aircraft initially gains energy in turns. Efficient high aspect-ratio
* aircraft (eg powered sailplanes) can use a lower value, whereas
* inefficient low aspect-ratio models (eg delta wings) can use a higher value.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_RLL2THR, 10.0f);
/**
* Speed <--> Altitude priority
*
* This parameter adjusts the amount of weighting that the pitch control
* applies to speed vs height errors. Setting it to 0.0 will cause the
* pitch control to control height and ignore speed errors. This will
* normally improve height accuracy but give larger airspeed errors.
* Setting it to 2.0 will cause the pitch control loop to control speed
* and ignore height errors. This will normally reduce airspeed errors,
* but give larger height errors. The default value of 1.0 allows the pitch
* control to simultaneously control height and speed.
* Note to Glider Pilots - set this parameter to 2.0 (The glider will
* adjust its pitch angle to maintain airspeed, ignoring changes in height).
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f);
/**
* Pitch damping factor
*
* This is the damping gain for the pitch demand loop. Increase to add
* damping to correct for oscillations in height. The default value of 0.0
* will work well provided the pitch to servo controller has been tuned
* properly.
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_PTCH_DAMP, 0.0f);
/**
* Height rate P factor
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_HRATE_P, 0.05f);
/**
* Speed rate P factor
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_T_SRATE_P, 0.05f);
/**
* Landing slope angle
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_ANG, 5.0f);
/**
* Landing slope length
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_SLLR, 0.9f);
/**
*
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_HVIRT, 10.0f);
/**
* Landing flare altitude (relative)
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_FLALT, 15.0f);
/**
* Landing throttle limit altitude (relative)
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_TLALT, 5.0f);
/**
* Landing heading hold horizontal distance
*
* @group L1 Control
*/
PARAM_DEFINE_FLOAT(FW_LND_HHDIST, 15.0f);
src/modules/mavlink/mavlink.c
+12
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@@ -72,8 +72,20 @@
// #include <uORB/topics/mission_result.h>
/* define MAVLink specific parameters */
/**
* MAVLink system ID
* @group MAVLink
*/
PARAM_DEFINE_INT32(MAV_SYS_ID, 1);
/**
* MAVLink component ID
* @group MAVLink
*/
PARAM_DEFINE_INT32(MAV_COMP_ID, 50);
/**
* MAVLink type
* @group MAVLink
*/
PARAM_DEFINE_INT32(MAV_TYPE, MAV_TYPE_FIXED_WING);
mavlink_system_t mavlink_system = {
src/modules/navigator/geofence_params.c
+11 -5
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@@ -45,11 +45,17 @@
#include <systemlib/param/param.h>
/*
* geofence parameters, accessible via MAVLink
*
* Geofence parameters, accessible via MAVLink
*/
// @DisplayName Switch to enable geofence
// @Description if set to 1 geofence is enabled, defaults to 1 because geofence is only enabled when the geofence.txt file is present
// @Range 0 or 1
/**
* Enable geofence.
*
* Set to 1 to enable geofence.
* Defaults to 1 because geofence is only enabled when the geofence.txt file is present.
*
* @min 0
* @max 1
* @group Geofence
*/
PARAM_DEFINE_INT32(GF_ON, 1);
src/modules/navigator/navigator_params.c
+60 -3
View File
@@ -50,15 +50,72 @@
/*
* Navigator parameters, accessible via MAVLink
*
*/
/**
* Minimum altitude
*
* @group Navigation
*/
PARAM_DEFINE_FLOAT(NAV_MIN_ALT, 50.0f);
/**
* Waypoint acceptance radius.
*
* @group Navigation
*/
PARAM_DEFINE_FLOAT(NAV_ACCEPT_RAD, 10.0f);
/**
* Loiter radius.
*
* @group Navigation
*/
PARAM_DEFINE_FLOAT(NAV_LOITER_RAD, 50.0f);
/**
* @group Navigation
*/
PARAM_DEFINE_INT32(NAV_ONB_MIS_EN, 0);
/**
* Default take-off altitude.
*
* @group Navigation
*/
PARAM_DEFINE_FLOAT(NAV_TAKEOFF_ALT, 10.0f); // default TAKEOFF altitude
/**
* Landing altitude.
*
* Slowly descend from this altitude when landing.
*
* @group Navigation
*/
PARAM_DEFINE_FLOAT(NAV_LAND_ALT, 5.0f); // slow descend from this altitude when landing
/**
* Return-to-land altitude.
*
* Minimum altitude for going home in RTL mode.
*
* @group Navigation
*/
PARAM_DEFINE_FLOAT(NAV_RTL_ALT, 30.0f); // min altitude for going home in RTL mode
PARAM_DEFINE_FLOAT(NAV_RTL_LAND_T, -1.0f); // delay after descend before landing, if set to -1 the system will not land but loiter at NAV_LAND_ALT
PARAM_DEFINE_INT32(NAV_PARACHUTE_EN, 0); // enable parachute deployment
/**
* Return-to-land delay.
*
* Delay after descend before landing.
* If set to -1 the system will not land but loiter at NAV_LAND_ALT.
*
* @group Navigation
*/
PARAM_DEFINE_FLOAT(NAV_RTL_LAND_T, -1.0f);
/**
* Enable parachute deployment.
*
* @group Navigation
*/
PARAM_DEFINE_INT32(NAV_PARACHUTE_EN, 0);
src/modules/sensors/sensor_params.c
+268 -35
View File
@@ -42,13 +42,10 @@
*/
#include <nuttx/config.h>
#include <systemlib/param/param.h>
/**
* Gyro X offset
*
* This is an X-axis offset for the gyro. Adjust it according to the calibration data.
* Gyro X-axis offset
*
* @min -10.0
* @max 10.0
@@ -57,7 +54,7 @@
PARAM_DEFINE_FLOAT(SENS_GYRO_XOFF, 0.0f);
/**
* Gyro Y offset
* Gyro Y-axis offset
*
* @min -10.0
* @max 10.0
@@ -66,7 +63,7 @@ PARAM_DEFINE_FLOAT(SENS_GYRO_XOFF, 0.0f);
PARAM_DEFINE_FLOAT(SENS_GYRO_YOFF, 0.0f);
/**
* Gyro Z offset
* Gyro Z-axis offset
*
* @min -5.0
* @max 5.0
@@ -75,9 +72,7 @@ PARAM_DEFINE_FLOAT(SENS_GYRO_YOFF, 0.0f);
PARAM_DEFINE_FLOAT(SENS_GYRO_ZOFF, 0.0f);
/**
* Gyro X scaling
*
* X-axis scaling.
* Gyro X-axis scaling factor
*
* @min -1.5
* @max 1.5
@@ -86,9 +81,7 @@ PARAM_DEFINE_FLOAT(SENS_GYRO_ZOFF, 0.0f);
PARAM_DEFINE_FLOAT(SENS_GYRO_XSCALE, 1.0f);
/**
* Gyro Y scaling
*
* Y-axis scaling.
* Gyro Y-axis scaling factor
*
* @min -1.5
* @max 1.5
@@ -97,9 +90,7 @@ PARAM_DEFINE_FLOAT(SENS_GYRO_XSCALE, 1.0f);
PARAM_DEFINE_FLOAT(SENS_GYRO_YSCALE, 1.0f);
/**
* Gyro Z scaling
*
* Z-axis scaling.
* Gyro Z-axis scaling factor
*
* @min -1.5
* @max 1.5
@@ -107,10 +98,9 @@ PARAM_DEFINE_FLOAT(SENS_GYRO_YSCALE, 1.0f);
*/
PARAM_DEFINE_FLOAT(SENS_GYRO_ZSCALE, 1.0f);
/**
* Magnetometer X offset
*
* This is an X-axis offset for the magnetometer.
* Magnetometer X-axis offset
*
* @min -500.0
* @max 500.0
@@ -119,9 +109,7 @@ PARAM_DEFINE_FLOAT(SENS_GYRO_ZSCALE, 1.0f);
PARAM_DEFINE_FLOAT(SENS_MAG_XOFF, 0.0f);
/**
* Magnetometer Y offset
*
* This is an Y-axis offset for the magnetometer.
* Magnetometer Y-axis offset
*
* @min -500.0
* @max 500.0
@@ -130,9 +118,7 @@ PARAM_DEFINE_FLOAT(SENS_MAG_XOFF, 0.0f);
PARAM_DEFINE_FLOAT(SENS_MAG_YOFF, 0.0f);
/**
* Magnetometer Z offset
*
* This is an Z-axis offset for the magnetometer.
* Magnetometer Z-axis offset
*
* @min -500.0
* @max 500.0
@@ -140,24 +126,134 @@ PARAM_DEFINE_FLOAT(SENS_MAG_YOFF, 0.0f);
*/
PARAM_DEFINE_FLOAT(SENS_MAG_ZOFF, 0.0f);
/**
* Magnetometer X-axis scaling factor
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_MAG_XSCALE, 1.0f);
/**
* Magnetometer Y-axis scaling factor
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_MAG_YSCALE, 1.0f);
/**
* Magnetometer Z-axis scaling factor
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_MAG_ZSCALE, 1.0f);
/**
* Accelerometer X-axis offset
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_ACC_XOFF, 0.0f);
/**
* Accelerometer Y-axis offset
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_ACC_YOFF, 0.0f);
/**
* Accelerometer Z-axis offset
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_ACC_ZOFF, 0.0f);
/**
* Accelerometer X-axis scaling factor
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_ACC_XSCALE, 1.0f);
/**
* Accelerometer Y-axis scaling factor
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_ACC_YSCALE, 1.0f);
/**
* Accelerometer Z-axis scaling factor
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_ACC_ZSCALE, 1.0f);
/**
* Differential pressure sensor offset
*
* @group Sensor Calibration
*/
PARAM_DEFINE_FLOAT(SENS_DPRES_OFF, 0.0f);
/**
* Differential pressure sensor analog enabled
*
* @group Sensor Calibration
*/
PARAM_DEFINE_INT32(SENS_DPRES_ANA, 0);
/**
* Board rotation
*
* This parameter defines the rotation of the FMU board relative to the platform.
* Possible values are:
* 0 = No rotation
* 1 = Yaw 45°
* 2 = Yaw 90°
* 3 = Yaw 135°
* 4 = Yaw 180°
* 5 = Yaw 225°
* 6 = Yaw 270°
* 7 = Yaw 315°
* 8 = Roll 180°
* 9 = Roll 180°, Yaw 45°
* 10 = Roll 180°, Yaw 90°
* 11 = Roll 180°, Yaw 135°
* 12 = Pitch 180°
* 13 = Roll 180°, Yaw 225°
* 14 = Roll 180°, Yaw 270°
* 15 = Roll 180°, Yaw 315°
* 16 = Roll 90°
* 17 = Roll 90°, Yaw 45°
* 18 = Roll 90°, Yaw 90°
* 19 = Roll 90°, Yaw 135°
* 20 = Roll 270°
* 21 = Roll 270°, Yaw 45°
* 22 = Roll 270°, Yaw 90°
* 23 = Roll 270°, Yaw 135°
* 24 = Pitch 90°
* 25 = Pitch 270°
*
* @group Sensor Calibration
*/
PARAM_DEFINE_INT32(SENS_BOARD_ROT, 0);
/**
* External magnetometer rotation
*
* This parameter defines the rotation of the external magnetometer relative
* to the platform (not relative to the FMU).
* See SENS_BOARD_ROT for possible values.
*
* @group Sensor Calibration
*/
PARAM_DEFINE_INT32(SENS_EXT_MAG_ROT, 0);
/**
* RC Channel 1 Minimum
*
@@ -367,20 +463,52 @@ PARAM_DEFINE_FLOAT(RC18_DZ, 0.0f);
#ifdef CONFIG_ARCH_BOARD_PX4FMU_V1
PARAM_DEFINE_INT32(RC_RL1_DSM_VCC, 0); /* Relay 1 controls DSM VCC */
#endif
PARAM_DEFINE_INT32(RC_DSM_BIND, -1); /* -1 = Idle, 0 = Start DSM2 bind, 1 = Start DSMX bind */
/**
* DSM binding trigger.
*
* -1 = Idle, 0 = Start DSM2 bind, 1 = Start DSMX bind
*
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_DSM_BIND, -1);
/**
* Scaling factor for battery voltage sensor on PX4IO.
*
* @group Battery Calibration
*/
PARAM_DEFINE_INT32(BAT_V_SCALE_IO, 10000);
#ifdef CONFIG_ARCH_BOARD_PX4FMU_V2
/**
* Scaling factor for battery voltage sensor on FMU v2.
*
* @group Battery Calibration
*/
PARAM_DEFINE_FLOAT(BAT_V_SCALING, 0.0082f);
#else
/* default is conversion factor for the PX4IO / PX4IOAR board, the factor for PX4FMU standalone is different */
/* PX4IOAR: 0.00838095238 */
/* FMU standalone: 1/(10 / (47+10)) * (3.3 / 4095) = 0.00459340659 */
/* FMU with PX4IOAR: (3.3f * 52.0f / 5.0f / 4095.0f) */
/**
* Scaling factor for battery voltage sensor on FMU v1.
*
* FMUv1 standalone: 1/(10 / (47+10)) * (3.3 / 4095) = 0.00459340659
* FMUv1 with PX4IO: 0.00459340659
* FMUv1 with PX4IOAR: (3.3f * 52.0f / 5.0f / 4095.0f) = 0.00838095238
*
* @group Battery Calibration
*/
PARAM_DEFINE_FLOAT(BAT_V_SCALING, 0.00459340659f);
#endif
/**
* Scaling factor for battery current sensor.
*
* @group Battery Calibration
*/
PARAM_DEFINE_FLOAT(BAT_C_SCALING, 0.0124); /* scaling for 3DR power brick */
/**
* Roll control channel mapping.
*
@@ -446,22 +574,127 @@ PARAM_DEFINE_INT32(RC_MAP_YAW, 4);
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_MODE_SW, 0);
/**
* Return switch channel mapping.
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_RETURN_SW, 0);
/**
* Assist switch channel mapping.
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_ASSIST_SW, 0);
/**
* Mission switch channel mapping.
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_MISSIO_SW, 0);
//PARAM_DEFINE_INT32(RC_MAP_OFFB_SW, 0);
/**
* Flaps channel mapping.
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_FLAPS, 0);
PARAM_DEFINE_INT32(RC_MAP_AUX1, 0); /**< default function: camera pitch */
PARAM_DEFINE_INT32(RC_MAP_AUX2, 0); /**< default function: camera roll */
PARAM_DEFINE_INT32(RC_MAP_AUX3, 0); /**< default function: camera azimuth / yaw */
/**
* Auxiliary switch 1 channel mapping.
*
* Default function: Camera pitch
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_AUX1, 0);
/**
* Auxiliary switch 2 channel mapping.
*
* Default function: Camera roll
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_AUX2, 0); /**< default function: camera roll */
/**
* Auxiliary switch 3 channel mapping.
*
* Default function: Camera azimuth / yaw
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_MAP_AUX3, 0);
/**
* Roll scaling factor
*
* @group Radio Calibration
*/
PARAM_DEFINE_FLOAT(RC_SCALE_ROLL, 0.6f);
/**
* Pitch scaling factor
*
* @group Radio Calibration
*/
PARAM_DEFINE_FLOAT(RC_SCALE_PITCH, 0.6f);
/**
* Yaw scaling factor
*
* @group Radio Calibration
*/
PARAM_DEFINE_FLOAT(RC_SCALE_YAW, 2.0f);
PARAM_DEFINE_INT32(RC_FS_CH, 0); /**< RC failsafe channel, 0 = disable */
PARAM_DEFINE_INT32(RC_FS_MODE, 0); /**< RC failsafe mode: 0 = too low means signal loss, 1 = too high means signal loss */
PARAM_DEFINE_FLOAT(RC_FS_THR, 800); /**< RC failsafe PWM threshold */
/**
* Failsafe channel mapping.
*
* @min 0
* @max 18
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_FS_CH, 0);
/**
* Failsafe channel mode.
*
* 0 = too low means signal loss,
* 1 = too high means signal loss
*
* @min 0
* @max 1
* @group Radio Calibration
*/
PARAM_DEFINE_INT32(RC_FS_MODE, 0);
/**
* Failsafe channel PWM threshold.
*
* @min 0
* @max 1
* @group Radio Calibration
*/
PARAM_DEFINE_FLOAT(RC_FS_THR, 800);
src/modules/systemlib/system_params.c
+17 -2
View File
@@ -40,8 +40,23 @@
#include <nuttx/config.h>
#include <systemlib/param/param.h>
// Auto-start script with index #n
/**
* Auto-start script index.
*
* Defines the auto-start script used to bootstrap the system.
*
* @group System
*/
PARAM_DEFINE_INT32(SYS_AUTOSTART, 0);
// Automatically configure default values
/**
* Automatically configure default values.
*
* Set to 1 to set platform-specific parameters to their default
* values on next system startup.
*
* @min 0
* @max 1
* @group System
*/
PARAM_DEFINE_INT32(SYS_AUTOCONFIG, 0);