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lines changed Original file line number Diff line number Diff line change @@ -205,7 +205,7 @@ PARAM_DEFINE_FLOAT(MC_PITCHRATE_K, 1.0f);
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*
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* @min 0.0
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* @max 0.6
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- * @decimal 2
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+ * @decimal 3
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* @increment 0.01
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* @group Multicopter Rate Control
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*/
@@ -217,7 +217,7 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_P, 0.2f);
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* Yaw rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
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*
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* @min 0.0
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- * @decimal 2
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+ * @decimal 3
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* @increment 0.01
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* @group Multicopter Rate Control
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*/
@@ -241,8 +241,8 @@ PARAM_DEFINE_FLOAT(MC_YR_INT_LIM, 0.30f);
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* Yaw rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
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*
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* @min 0.0
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- * @decimal 2
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- * @increment 0.01
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+ * @decimal 4
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+ * @increment 0.0005
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* @group Multicopter Rate Control
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*/
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PARAM_DEFINE_FLOAT (MC_YAWRATE_D , 0.0f );
@@ -254,7 +254,6 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f);
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*
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* @min 0.0
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* @decimal 4
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- * @increment 0.01
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* @group Multicopter Rate Control
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*/
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PARAM_DEFINE_FLOAT (MC_YAWRATE_FF , 0.0f );
@@ -271,7 +270,7 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_FF, 0.0f);
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* Set MC_YAWRATE_P=1 to implement a PID in the ideal form.
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* Set MC_YAWRATE_K=1 to implement a PID in the parallel form.
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*
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- * @min 0.0
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+ * @min 0.01
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* @max 5.0
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* @decimal 4
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* @increment 0.0005
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