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-rw-r--r--src/modules/mc_att_control/mc_att_control_params.c48
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);