diff options
Diffstat (limited to 'src/modules/fw_pos_control_l1/mtecs/mTecs_params.c')
| -rw-r--r-- | src/modules/fw_pos_control_l1/mtecs/mTecs_params.c | 88 |
1 files changed, 44 insertions, 44 deletions
diff --git a/src/modules/fw_pos_control_l1/mtecs/mTecs_params.c b/src/modules/fw_pos_control_l1/mtecs/mTecs_params.c index 58a1e9f6b..fff506865 100644 --- a/src/modules/fw_pos_control_l1/mtecs/mTecs_params.c +++ b/src/modules/fw_pos_control_l1/mtecs/mTecs_params.c @@ -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); |