group l1 control and tecs as FW

src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c

@@ -54,7 +54,7 @@
  * @unit m
  * @min 12.0
  * @max 50.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_L1_PERIOD, 20.0f);
 
@@ -65,7 +65,7 @@ PARAM_DEFINE_FLOAT(FW_L1_PERIOD, 20.0f);
  *
  * @min 0.6
  * @max 0.9
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_L1_DAMPING, 0.75f);
 
@@ -76,7 +76,7 @@ PARAM_DEFINE_FLOAT(FW_L1_DAMPING, 0.75f);
  *
  * @min 0.0
  * @max 1.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_THR_CRUISE, 0.6f);
 
@@ -87,7 +87,7 @@ PARAM_DEFINE_FLOAT(FW_THR_CRUISE, 0.6f);
  *
  * @min 0.0
  * @max 1.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_THR_SLEW_MAX, 0.0f);
 
@@ -99,7 +99,7 @@ PARAM_DEFINE_FLOAT(FW_THR_SLEW_MAX, 0.0f);
  * @unit deg
  * @min -60.0
  * @max 0.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_P_LIM_MIN, -45.0f);
 
@@ -111,7 +111,7 @@ PARAM_DEFINE_FLOAT(FW_P_LIM_MIN, -45.0f);
  * @unit deg
  * @min 0.0
  * @max 60.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_P_LIM_MAX, 45.0f);
 
@@ -123,7 +123,7 @@ PARAM_DEFINE_FLOAT(FW_P_LIM_MAX, 45.0f);
  * @unit deg
  * @min 35.0
  * @max 65.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_R_LIM, 50.0f);
 
@@ -136,7 +136,7 @@ PARAM_DEFINE_FLOAT(FW_R_LIM, 50.0f);
  *
  * @min 0.0
  * @max 1.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_THR_MAX, 1.0f);
 
@@ -154,7 +154,7 @@ PARAM_DEFINE_FLOAT(FW_THR_MAX, 1.0f);
  *
  * @min 0.0
  * @max 1.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
 
@@ -168,7 +168,7 @@ PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
  *
  * @min 0.0
  * @max 0.4
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_THR_IDLE, 0.15f);
 
@@ -180,7 +180,7 @@ PARAM_DEFINE_FLOAT(FW_THR_IDLE, 0.15f);
  *
  * @min 0.0
  * @max 1.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_THR_LND_MAX, 1.0f);
 
@@ -195,7 +195,7 @@ PARAM_DEFINE_FLOAT(FW_THR_LND_MAX, 1.0f);
  * @unit m
  * @min 0.0
  * @max 150.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_CLMBOUT_DIFF, 10.0f);
 
@@ -218,7 +218,7 @@ PARAM_DEFINE_FLOAT(FW_CLMBOUT_DIFF, 10.0f);
  * @unit m/s
  * @min 2.0
  * @max 10.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_T_CLMB_MAX, 5.0f);
 
@@ -230,7 +230,7 @@ PARAM_DEFINE_FLOAT(FW_T_CLMB_MAX, 5.0f);
  * to measure FW_T_CLMB_MAX.
  *
  * @unit m/s
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_SINK_MIN, 2.0f);
 
@@ -244,7 +244,7 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MIN, 2.0f);
  * the aircraft.
  *
  * @unit m/s
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f);
 
@@ -256,7 +256,7 @@ PARAM_DEFINE_FLOAT(FW_T_SINK_MAX, 5.0f);
  * to respond.
  *
  * @unit s
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_TIME_CONST, 5.0f);
 
@@ -268,7 +268,7 @@ PARAM_DEFINE_FLOAT(FW_T_TIME_CONST, 5.0f);
  * to respond.
  *
  * @unit s
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_THRO_CONST, 8.0f);
 
@@ -278,7 +278,7 @@ PARAM_DEFINE_FLOAT(FW_T_THRO_CONST, 8.0f);
  * This is the damping gain for the throttle demand loop.
  * Increase to add damping to correct for oscillations in speed and height.
  *
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f);
 
@@ -290,7 +290,7 @@ PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.5f);
  * and height offsets are trimmed out, but reduces damping and
  * increases overshoot.
  *
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f);
 
@@ -304,7 +304,7 @@ PARAM_DEFINE_FLOAT(FW_T_INTEG_GAIN, 0.1f);
  * from under-speed conditions.
  *
  * @unit m/s/s
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_VERT_ACC, 7.0f);
 
@@ -318,7 +318,7 @@ PARAM_DEFINE_FLOAT(FW_T_VERT_ACC, 7.0f);
  * the solution more towards use of the accelerometer data.
  *
  * @unit rad/s
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_HGT_OMEGA, 3.0f);
 
@@ -332,7 +332,7 @@ PARAM_DEFINE_FLOAT(FW_T_HGT_OMEGA, 3.0f);
  * solution more towards use of the accelerometer data.
  *
  * @unit rad/s
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_SPD_OMEGA, 2.0f);
 
@@ -348,7 +348,7 @@ PARAM_DEFINE_FLOAT(FW_T_SPD_OMEGA, 2.0f);
  * aircraft (eg powered sailplanes) can use a lower value, whereas
  * inefficient low aspect-ratio models (eg delta wings) can use a higher value.
  *
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_RLL2THR, 15.0f);
 
@@ -368,7 +368,7 @@ PARAM_DEFINE_FLOAT(FW_T_RLL2THR, 15.0f);
  *
  * @min 0.0
  * @max 2.0
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f);
 
@@ -380,28 +380,28 @@ PARAM_DEFINE_FLOAT(FW_T_SPDWEIGHT, 1.0f);
  * will work well provided the pitch to servo controller has been tuned
  * properly.
  *
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_PTCH_DAMP, 0.0f);
 
 /**
  * Height rate P factor
  *
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_HRATE_P, 0.05f);
 
 /**
  * Height rate FF factor
  *
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.0f);
 
 /**
  * Speed rate P factor
  *
- * @group Fixed Wing TECS
+ * @group FW TECS
  */
 PARAM_DEFINE_FLOAT(FW_T_SRATE_P, 0.02f);
 
@@ -411,7 +411,7 @@ PARAM_DEFINE_FLOAT(FW_T_SRATE_P, 0.02f);
  * @unit deg
  * @min 1.0
  * @max 15.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_LND_ANG, 5.0f);
 
@@ -419,7 +419,7 @@ PARAM_DEFINE_FLOAT(FW_LND_ANG, 5.0f);
  *
  *
  * @unit m
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_LND_HVIRT, 10.0f);
 
@@ -429,7 +429,7 @@ PARAM_DEFINE_FLOAT(FW_LND_HVIRT, 10.0f);
  * @unit m
  * @min 0.0
  * @max 25.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_LND_FLALT, 8.0f);
 
@@ -442,7 +442,7 @@ PARAM_DEFINE_FLOAT(FW_LND_FLALT, 8.0f);
  * @unit m
  * @min -1.0
  * @max 30.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_LND_TLALT, -1.0f);
 
@@ -452,7 +452,7 @@ PARAM_DEFINE_FLOAT(FW_LND_TLALT, -1.0f);
  * @unit m
  * @min 0
  * @max 30.0
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_LND_HHDIST, 15.0f);
 
@@ -462,7 +462,7 @@ PARAM_DEFINE_FLOAT(FW_LND_HHDIST, 15.0f);
  * 0: disabled, 1: enabled
  *
  * @unit boolean
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_INT32(FW_LND_USETER, 0);
 
@@ -475,7 +475,7 @@ PARAM_DEFINE_INT32(FW_LND_USETER, 0);
  * @unit deg
  * @min 0
  * @max 15.0
- * @group L1 Control
+ * @group FW L1 Control
  *
  */
 PARAM_DEFINE_FLOAT(FW_LND_FL_PMIN, 2.5f);
@@ -489,7 +489,7 @@ PARAM_DEFINE_FLOAT(FW_LND_FL_PMIN, 2.5f);
  * @unit deg
  * @min 0
  * @max 45.0
- * @group L1 Control
+ * @group FW L1 Control
  *
  */
 PARAM_DEFINE_FLOAT(FW_LND_FL_PMAX, 15.0f);
@@ -502,6 +502,6 @@ PARAM_DEFINE_FLOAT(FW_LND_FL_PMAX, 15.0f);
  *
  * @min 1.0
  * @max 1.5
- * @group L1 Control
+ * @group FW L1 Control
  */
 PARAM_DEFINE_FLOAT(FW_LND_AIRSPD_SC, 1.3f);