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/**
* @file mc_att_control_params.c
* Parameters for multicopter attitude controller.
*
* @author Tobias Naegeli <naegelit@student.ethz.ch>
* @author Lorenz Meier <lm@inf.ethz.ch>
* @author Anton Babushkin <anton.babushkin@me.com>
*/
#include <px4_defines.h>
#include "mc_att_control_params.h"
#include <systemlib/param/param.h>
/**
* Roll P gain
*
* Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_ROLL_P);
/**
* Roll rate P gain
*
* Roll rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_ROLLRATE_P);
/**
* Roll rate I gain
*
* Roll rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_ROLLRATE_I);
/**
* Roll rate D gain
*
* Roll rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_ROLLRATE_D);
/**
* Pitch P gain
*
* Pitch proportional gain, i.e. desired angular speed in rad/s for error 1 rad.
*
* @unit 1/s
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_PITCH_P);
/**
* Pitch rate P gain
*
* Pitch rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_PITCHRATE_P);
/**
* Pitch rate I gain
*
* Pitch rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_PITCHRATE_I);
/**
* Pitch rate D gain
*
* Pitch rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_PITCHRATE_D);
/**
* Yaw P gain
*
* Yaw proportional gain, i.e. desired angular speed in rad/s for error 1 rad.
*
* @unit 1/s
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_YAW_P);
/**
* Yaw rate P gain
*
* Yaw rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_YAWRATE_P);
/**
* Yaw rate I gain
*
* Yaw rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_YAWRATE_I);
/**
* Yaw rate D gain
*
* Yaw rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_YAWRATE_D);
/**
* Yaw feed forward
*
* Feed forward weight for manual yaw control. 0 will give slow responce and no overshot, 1 - fast responce and big overshot.
*
* @min 0.0
* @max 1.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_YAW_FF);
/**
* Max yaw rate
*
* Limit for yaw rate, has effect for large rotations in autonomous mode, to avoid large control output and mixer saturation.
*
* @unit deg/s
* @min 0.0
* @max 360.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_YAWRATE_MAX);
/**
* Max manual roll
*
* @unit deg
* @min 0.0
* @max 90.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_MAN_R_MAX);
/**
* Max manual pitch
*
* @unit deg
* @min 0.0
* @max 90.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_MAN_P_MAX);
/**
* Max manual yaw rate
*
* @unit deg/s
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_MAN_Y_MAX);
/**
* Max acro roll rate
*
* @unit deg/s
* @min 0.0
* @max 360.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_ACRO_R_MAX);
/**
* Max acro pitch rate
*
* @unit deg/s
* @min 0.0
* @max 360.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_ACRO_P_MAX);
/**
* Max acro yaw rate
*
* @unit deg/s
* @min 0.0
* @group Multicopter Attitude Control
*/
PX4_PARAM_DEFINE_FLOAT(MC_ACRO_Y_MAX);
