diff options
author | Lorenz Meier <lm@inf.ethz.ch> | 2014-07-06 15:47:34 +0200 |
---|---|---|
committer | Lorenz Meier <lm@inf.ethz.ch> | 2014-07-06 15:47:34 +0200 |
commit | 1492323f0327916435d806c2af1e0c8296278c9d (patch) | |
tree | d53e2768c326ec6a2cbcfd896550c446ba93fab3 /src/modules/mc_att_control/mc_att_control_params.c | |
parent | 2669f7f3af65921d4abbf3850cd62e48f2eeeec7 (diff) | |
parent | bd88951f6ce609bc5ba364bfa3d19ae61e444964 (diff) | |
download | px4-firmware-1492323f0327916435d806c2af1e0c8296278c9d.tar.gz px4-firmware-1492323f0327916435d806c2af1e0c8296278c9d.tar.bz2 px4-firmware-1492323f0327916435d806c2af1e0c8296278c9d.zip |
Merged master into uavcan
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 | 48 |
1 files changed, 45 insertions, 3 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 e52c39368..819847b40 100644 --- a/src/modules/mc_att_control/mc_att_control_params.c +++ b/src/modules/mc_att_control/mc_att_control_params.c @@ -1,9 +1,6 @@ /**************************************************************************** * * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. - * Author: @author Tobias Naegeli <naegelit@student.ethz.ch> - * @author Lorenz Meier <lm@inf.ethz.ch> - * @author Anton Babushkin <anton.babushkin@me.com> * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -37,6 +34,10 @@ /** * @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 <systemlib/param/param.h> @@ -175,6 +176,18 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f); PARAM_DEFINE_FLOAT(MC_YAW_FF, 0.5f); /** + * 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 + */ +PARAM_DEFINE_FLOAT(MC_YAWRATE_MAX, 120.0f); + +/** * Max manual roll * * @unit deg @@ -202,3 +215,32 @@ PARAM_DEFINE_FLOAT(MC_MAN_P_MAX, 35.0f); * @group Multicopter Attitude Control */ PARAM_DEFINE_FLOAT(MC_MAN_Y_MAX, 120.0f); + +/** + * Max acro roll rate + * + * @unit deg/s + * @min 0.0 + * @max 360.0 + * @group Multicopter Attitude Control + */ +PARAM_DEFINE_FLOAT(MC_ACRO_R_MAX, 90.0f); + +/** + * Max acro pitch rate + * + * @unit deg/s + * @min 0.0 + * @max 360.0 + * @group Multicopter Attitude Control + */ +PARAM_DEFINE_FLOAT(MC_ACRO_P_MAX, 90.0f); + +/** + * Max acro yaw rate + * + * @unit deg/s + * @min 0.0 + * @group Multicopter Attitude Control + */ +PARAM_DEFINE_FLOAT(MC_ACRO_Y_MAX, 120.0f); |