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TECS: update some params to latest results from flight testing

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
release/1.12
Silvan Fuhrer 4 years ago committed by Roman Bapst
parent
commit
3d3ff75495
  1. 6
      src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c

6
src/modules/fw_pos_control_l1/fw_pos_control_l1_params.c

@ -549,7 +549,7 @@ PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.1f); @@ -549,7 +549,7 @@ PARAM_DEFINE_FLOAT(FW_T_THR_DAMP, 0.1f);
* @increment 0.05
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_I_GAIN_THR, 0.1f);
PARAM_DEFINE_FLOAT(FW_T_I_GAIN_THR, 0.3f);
/**
* Integrator gain pitch
@ -681,7 +681,7 @@ PARAM_DEFINE_FLOAT(FW_T_ALT_TC, 5.0f); @@ -681,7 +681,7 @@ PARAM_DEFINE_FLOAT(FW_T_ALT_TC, 5.0f);
* @increment 0.05
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.4f);
PARAM_DEFINE_FLOAT(FW_T_HRATE_FF, 0.3f);
/**
* True airspeed error time constant.
@ -746,4 +746,4 @@ PARAM_DEFINE_FLOAT(FW_T_STE_R_TC, 0.4f); @@ -746,4 +746,4 @@ PARAM_DEFINE_FLOAT(FW_T_STE_R_TC, 0.4f);
* @increment 0.01
* @group FW TECS
*/
PARAM_DEFINE_FLOAT(FW_T_TAS_R_TC, 0.05f);
PARAM_DEFINE_FLOAT(FW_T_TAS_R_TC, 0.2f);

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