diff options
Diffstat (limited to 'src/modules/mc_att_control/mc_att_control_params.c')
| -rw-r--r-- | src/modules/mc_att_control/mc_att_control_params.c | 119 |
1 files changed, 119 insertions, 0 deletions
diff --git a/src/modules/mc_att_control/mc_att_control_params.c b/src/modules/mc_att_control/mc_att_control_params.c index f3a4022c8..56b61a88b 100644 --- a/src/modules/mc_att_control/mc_att_control_params.c +++ b/src/modules/mc_att_control/mc_att_control_params.c @@ -41,18 +41,137 @@ #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 + */ PARAM_DEFINE_FLOAT(MC_ROLL_P, 6.0f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_ROLLRATE_P, 0.1f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_ROLLRATE_I, 0.0f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_ROLLRATE_D, 0.002f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_PITCH_P, 6.0f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_PITCHRATE_P, 0.1f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_PITCHRATE_I, 0.0f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_PITCHRATE_D, 0.002f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_YAW_P, 2.0f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_YAWRATE_P, 0.3f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_YAWRATE_I, 0.0f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f); + +/** + * 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 + */ PARAM_DEFINE_FLOAT(MC_YAW_FF, 0.5f); PARAM_DEFINE_FLOAT(MC_ROLL_S_ACRO, 5.0f); PARAM_DEFINE_FLOAT(MC_PITCH_S_ACRO, 5.0f); |