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Clean up parameter meta data as needed by QGC

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This commit is contained in:
Don Gagne
2015-04-14 23:26:14 -07:00
parent c8452bb9d6
commit 3dc8cf8769
6 changed files with 61 additions and 62 deletions
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src/modules/commander/commander_params.c
+6 -6
View File
@@ -139,8 +139,8 @@ PARAM_DEFINE_INT32(COM_DL_REG_T, 0);
* Engine failure triggers only above this throttle value
*
* @group commander
* @min 0.0f
* @max 1.0f
* @min 0.0
* @max 1.0
*/
PARAM_DEFINE_FLOAT(COM_EF_THROT, 0.5f);
@@ -149,8 +149,8 @@ PARAM_DEFINE_FLOAT(COM_EF_THROT, 0.5f);
* Engine failure triggers only below this current/throttle value
*
* @group commander
* @min 0.0f
* @max 7.0f
* @min 0.0
* @max 7.0
*/
PARAM_DEFINE_FLOAT(COM_EF_C2T, 5.0f);
@@ -161,8 +161,8 @@ PARAM_DEFINE_FLOAT(COM_EF_C2T, 5.0f);
*
* @group commander
* @unit second
* @min 0.0f
* @max 7.0f
* @min 0.0
* @max 7.0
*/
PARAM_DEFINE_FLOAT(COM_EF_TIME, 10.0f);
src/modules/fw_pos_control_l1/mtecs/mTecs_params.c
+44 -44
View File
@@ -157,8 +157,8 @@ PARAM_DEFINE_FLOAT(MT_THR_MAX, 1.0f);
/**
* Minimal Pitch Setpoint in Degrees
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -167,8 +167,8 @@ PARAM_DEFINE_FLOAT(MT_PIT_MIN, -45.0f);
/**
* Maximal Pitch Setpoint in Degrees
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -192,8 +192,8 @@ PARAM_DEFINE_FLOAT(MT_FPA_LP, 1.0f);
* P gain for the altitude control
* Maps the altitude error to the flight path angle setpoint
*
* @min 0.0f
* @max 10.0f
* @min 0.0
* @max 10.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_FPA_P, 0.3f);
@@ -202,8 +202,8 @@ PARAM_DEFINE_FLOAT(MT_FPA_P, 0.3f);
* D gain for the altitude control
* Maps the change of altitude error to the flight path angle setpoint
*
* @min 0.0f
* @max 10.0f
* @min 0.0
* @max 10.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_FPA_D, 0.0f);
@@ -219,8 +219,8 @@ PARAM_DEFINE_FLOAT(MT_FPA_D_LP, 1.0f);
/**
* Minimal flight path angle setpoint
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -229,8 +229,8 @@ PARAM_DEFINE_FLOAT(MT_FPA_MIN, -20.0f);
/**
* Maximal flight path angle setpoint
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -254,8 +254,8 @@ PARAM_DEFINE_FLOAT(MT_AD_LP, 0.5f);
* P gain for the airspeed control
* Maps the airspeed error to the acceleration setpoint
*
* @min 0.0f
* @max 10.0f
* @min 0.0
* @max 10.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_ACC_P, 0.3f);
@@ -264,8 +264,8 @@ PARAM_DEFINE_FLOAT(MT_ACC_P, 0.3f);
* D gain for the airspeed control
* Maps the change of airspeed error to the acceleration setpoint
*
* @min 0.0f
* @max 10.0f
* @min 0.0
* @max 10.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_ACC_D, 0.0f);
@@ -296,8 +296,8 @@ PARAM_DEFINE_FLOAT(MT_ACC_MAX, 40.0f);
/**
* Minimal throttle during takeoff
*
* @min 0.0f
* @max 1.0f
* @min 0.0
* @max 1.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_TKF_THR_MIN, 1.0f);
@@ -305,8 +305,8 @@ PARAM_DEFINE_FLOAT(MT_TKF_THR_MIN, 1.0f);
/**
* Maximal throttle during takeoff
*
* @min 0.0f
* @max 1.0f
* @min 0.0
* @max 1.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_TKF_THR_MAX, 1.0f);
@@ -314,8 +314,8 @@ PARAM_DEFINE_FLOAT(MT_TKF_THR_MAX, 1.0f);
/**
* Minimal pitch during takeoff
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -324,8 +324,8 @@ PARAM_DEFINE_FLOAT(MT_TKF_PIT_MIN, 0.0f);
/**
* Maximal pitch during takeoff
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -334,8 +334,8 @@ PARAM_DEFINE_FLOAT(MT_TKF_PIT_MAX, 45.0f);
/**
* Minimal throttle in underspeed mode
*
* @min 0.0f
* @max 1.0f
* @min 0.0
* @max 1.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_USP_THR_MIN, 1.0f);
@@ -343,8 +343,8 @@ PARAM_DEFINE_FLOAT(MT_USP_THR_MIN, 1.0f);
/**
* Maximal throttle in underspeed mode
*
* @min 0.0f
* @max 1.0f
* @min 0.0
* @max 1.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_USP_THR_MAX, 1.0f);
@@ -352,8 +352,8 @@ PARAM_DEFINE_FLOAT(MT_USP_THR_MAX, 1.0f);
/**
* Minimal pitch in underspeed mode
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -362,8 +362,8 @@ PARAM_DEFINE_FLOAT(MT_USP_PIT_MIN, -45.0f);
/**
* Maximal pitch in underspeed mode
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -372,8 +372,8 @@ PARAM_DEFINE_FLOAT(MT_USP_PIT_MAX, 0.0f);
/**
* Minimal throttle in landing mode (only last phase of landing)
*
* @min 0.0f
* @max 1.0f
* @min 0.0
* @max 1.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_LND_THR_MIN, 0.0f);
@@ -381,8 +381,8 @@ PARAM_DEFINE_FLOAT(MT_LND_THR_MIN, 0.0f);
/**
* Maximal throttle in landing mode (only last phase of landing)
*
* @min 0.0f
* @max 1.0f
* @min 0.0
* @max 1.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_LND_THR_MAX, 0.0f);
@@ -390,8 +390,8 @@ PARAM_DEFINE_FLOAT(MT_LND_THR_MAX, 0.0f);
/**
* Minimal pitch in landing mode
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -400,8 +400,8 @@ PARAM_DEFINE_FLOAT(MT_LND_PIT_MIN, -5.0f);
/**
* Maximal pitch in landing mode
*
* @min -90.0f
* @max 90.0f
* @min -90.0
* @max 90.0
* @unit deg
* @group mTECS
*/
@@ -410,8 +410,8 @@ PARAM_DEFINE_FLOAT(MT_LND_PIT_MAX, 15.0f);
/**
* Integrator Limit for Total Energy Rate Control
*
* @min 0.0f
* @max 10.0f
* @min 0.0
* @max 10.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_THR_I_MAX, 10.0f);
@@ -419,8 +419,8 @@ PARAM_DEFINE_FLOAT(MT_THR_I_MAX, 10.0f);
/**
* Integrator Limit for Energy Distribution Rate Control
*
* @min 0.0f
* @max 10.0f
* @min 0.0
* @max 10.0
* @group mTECS
*/
PARAM_DEFINE_FLOAT(MT_PIT_I_MAX, 10.0f);
src/modules/navigator/datalinkloss_params.c
+2 -2
View File
@@ -64,7 +64,7 @@ PARAM_DEFINE_FLOAT(NAV_DLL_CH_T, 120.0f);
* Latitude of comms hold waypoint
*
* @unit degrees * 1e7
* @min 0.0
* @min 0
* @group DLL
*/
PARAM_DEFINE_INT32(NAV_DLL_CH_LAT, -266072120);
@@ -75,7 +75,7 @@ PARAM_DEFINE_INT32(NAV_DLL_CH_LAT, -266072120);
* Longitude of comms hold waypoint
*
* @unit degrees * 1e7
* @min 0.0
* @min 0
* @group DLL
*/
PARAM_DEFINE_INT32(NAV_DLL_CH_LON, 1518453890);
src/modules/navigator/navigator_params.c
+2 -2
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@@ -94,7 +94,7 @@ PARAM_DEFINE_INT32(NAV_RCL_OBC, 0);
* Latitude of airfield home waypoint
*
* @unit degrees * 1e7
* @min 0.0
* @min 0
* @group DLL
*/
PARAM_DEFINE_INT32(NAV_AH_LAT, -265847810);
@@ -105,7 +105,7 @@ PARAM_DEFINE_INT32(NAV_AH_LAT, -265847810);
* Longitude of airfield home waypoint
*
* @unit degrees * 1e7
* @min 0.0
* @min 0
* @group DLL
*/
PARAM_DEFINE_INT32(NAV_AH_LON, 1518423250);
src/modules/position_estimator_inav/position_estimator_inav_params.c
+4 -5
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@@ -282,8 +282,8 @@ PARAM_DEFINE_FLOAT(INAV_DELAY_GPS, 0.2f);
*
* Set to the appropriate key (328754) to disable vision input.
*
* @min 0.0
* @max 1.0
* @min 0
* @max 1
* @group Position Estimator INAV
*/
PARAM_DEFINE_INT32(CBRK_NO_VISION, 0);
@@ -295,9 +295,8 @@ PARAM_DEFINE_INT32(CBRK_NO_VISION, 0);
* the system uses the combined attitude / position
* filter framework.
*
* @min 0.0
* @max 1.0
* @unit s
* @min 0
* @max 1
* @group Position Estimator INAV
*/
PARAM_DEFINE_INT32(INAV_ENABLED, 1);
src/modules/vtol_att_control/vtol_att_control_params.c
+3 -3
View File
@@ -43,7 +43,7 @@
/**
* VTOL number of engines
*
* @min 1.0
* @min 1
* @group VTOL Attitude Control
*/
PARAM_DEFINE_INT32(VT_MOT_COUNT,0);
@@ -92,8 +92,8 @@ PARAM_DEFINE_FLOAT(VT_MC_ARSPD_TRIM,10.0f);
* If set to one this parameter will cause permanent attitude stabilization in fw mode.
* This parameter has been introduced for pure convenience sake.
*
* @min 0.0
* @max 1.0
* @min 0
* @max 1
* @group VTOL Attitude Control
*/
PARAM_DEFINE_INT32(VT_FW_PERM_STAB,0);