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param remove empty @unit

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This commit is contained in:
Daniel Agar
2016-03-14 09:12:34 +01:00
committed by Lorenz Meier
parent 146cdf578a
commit 7a9427bc34
27 changed files with 0 additions and 195 deletions
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src/modules/mc_att_control_multiplatform/mc_att_control_params.c
-11
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@@ -45,7 +45,6 @@
*
* Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad.
*
* @unit
* @min 0.0
* @group Multicopter Attitude Control
*/
@@ -56,7 +55,6 @@ 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
*/
@@ -67,7 +65,6 @@ 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
*/
@@ -78,7 +75,6 @@ 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
*/
@@ -100,7 +96,6 @@ 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
*/
@@ -111,7 +106,6 @@ 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
*/
@@ -122,7 +116,6 @@ 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
*/
@@ -144,7 +137,6 @@ 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
*/
@@ -155,7 +147,6 @@ 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
*/
@@ -166,7 +157,6 @@ 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
*/
@@ -177,7 +167,6 @@ 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