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 | 25 |
1 files changed, 16 insertions, 9 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 5b9238780..7cfe63fbc 100644 --- a/src/modules/fw_pos_control_l1/mtecs/mTecs_params.c +++ b/src/modules/fw_pos_control_l1/mtecs/mTecs_params.c @@ -175,6 +175,13 @@ PARAM_DEFINE_FLOAT(MT_PIT_MIN, -45.0f); PARAM_DEFINE_FLOAT(MT_PIT_MAX, 20.0f); /** + * Lowpass (cutoff freq.) for altitude + * + * @group mTECS + */ +PARAM_DEFINE_FLOAT(MT_ALT_LP, 1.0f); + +/** * Lowpass (cutoff freq.) for the flight path angle * * @group mTECS @@ -234,7 +241,14 @@ PARAM_DEFINE_FLOAT(MT_FPA_MAX, 30.0f); * * @group mTECS */ -PARAM_DEFINE_FLOAT(MT_A_LP, 1.0f); +PARAM_DEFINE_FLOAT(MT_A_LP, 0.5f); + +/** + * Airspeed derivative calculation lowpass + * + * @group mTECS + */ +PARAM_DEFINE_FLOAT(MT_AD_LP, 0.5f); /** * P gain for the airspeed control @@ -261,7 +275,7 @@ PARAM_DEFINE_FLOAT(MT_ACC_D, 0.0f); * * @group mTECS */ -PARAM_DEFINE_FLOAT(MT_ACC_D_LP, 1.0f); +PARAM_DEFINE_FLOAT(MT_ACC_D_LP, 0.5f); /** * Minimal acceleration (air) @@ -280,13 +294,6 @@ PARAM_DEFINE_FLOAT(MT_ACC_MIN, -40.0f); PARAM_DEFINE_FLOAT(MT_ACC_MAX, 40.0f); /** - * Airspeed derivative calculation lowpass - * - * @group mTECS - */ -PARAM_DEFINE_FLOAT(MT_AD_LP, 1.0f); - -/** * Minimal throttle during takeoff * * @min 0.0f |