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mc_att_control_multiplatform param @unit

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Daniel Agar
2016-03-14 09:10:29 +01:00
committed by Lorenz Meier
parent 55b33e97b3
commit 018c6cec76
1 changed files with 11 additions and 0 deletions
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src/modules/mc_att_control_multiplatform/mc_att_control_params.c
+11
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@@ -45,6 +45,7 @@
*
* Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -55,6 +56,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_ROLL_P);
*
* Roll rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -65,6 +67,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_ROLLRATE_P);
*
* Roll rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -75,6 +78,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_ROLLRATE_I);
*
* Roll rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -96,6 +100,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_PITCH_P);
*
* Pitch rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -106,6 +111,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_PITCHRATE_P);
*
* Pitch rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -116,6 +122,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_PITCHRATE_I);
*
* Pitch rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -137,6 +144,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAW_P);
*
* Yaw rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -147,6 +155,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAWRATE_P);
*
* Yaw rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -157,6 +166,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAWRATE_I);
*
* Yaw rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -167,6 +177,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAWRATE_D);
*
* Feed forward weight for manual yaw control. 0 will give slow responce and no overshot, 1 - fast responce and big overshot.
*
* @unit
* @min 0.0
* @max 1.0
* @group Multicopter Attitude Control