diff options
Diffstat (limited to 'apps/examples/control_demo')
-rw-r--r-- | apps/examples/control_demo/params.c | 44 |
1 files changed, 22 insertions, 22 deletions
diff --git a/apps/examples/control_demo/params.c b/apps/examples/control_demo/params.c index 8f923f5a1..6525b70f5 100644 --- a/apps/examples/control_demo/params.c +++ b/apps/examples/control_demo/params.c @@ -14,50 +14,50 @@ PARAM_DEFINE_FLOAT(FWB_R_LP, 300.0f); // yaw rate low pass cut freq PARAM_DEFINE_FLOAT(FWB_R_HP, 1.0f); // yaw rate high pass // stabilization mode -PARAM_DEFINE_FLOAT(FWB_P2AIL, 0.5f); // roll rate 2 aileron -PARAM_DEFINE_FLOAT(FWB_Q2ELV, 0.5f); // pitch rate 2 elevator -PARAM_DEFINE_FLOAT(FWB_R2RDR, 0.2f); // yaw rate 2 rudder +PARAM_DEFINE_FLOAT(FWB_P2AIL, 0.3f); // roll rate 2 aileron +PARAM_DEFINE_FLOAT(FWB_Q2ELV, 0.1f); // pitch rate 2 elevator +PARAM_DEFINE_FLOAT(FWB_R2RDR, 0.1f); // yaw rate 2 rudder // psi -> phi -> p PARAM_DEFINE_FLOAT(FWB_PSI2PHI, 0.5f); // heading 2 roll PARAM_DEFINE_FLOAT(FWB_PHI2P, 1.0f); // roll to roll rate -PARAM_DEFINE_FLOAT(FWB_PHI_LIM_MAX, 0.5f); // roll limit, 28 deg +PARAM_DEFINE_FLOAT(FWB_PHI_LIM_MAX, 0.3f); // roll limit, 28 deg // velocity -> theta -PARAM_DEFINE_FLOAT(FWB_V2THE_P, 0.2f); -PARAM_DEFINE_FLOAT(FWB_V2THE_I, 0.0f); -PARAM_DEFINE_FLOAT(FWB_V2THE_D, 0.0f); -PARAM_DEFINE_FLOAT(FWB_V2THE_D_LP, 0.0f); -PARAM_DEFINE_FLOAT(FWB_V2THE_I_MAX, 0.0f); -PARAM_DEFINE_FLOAT(FWB_THE_MIN, -0.5f); -PARAM_DEFINE_FLOAT(FWB_THE_MAX, 0.5f); +PARAM_DEFINE_FLOAT(FWB_V2THE_P, 1.0f); // velocity to pitch angle PID, prop gain +PARAM_DEFINE_FLOAT(FWB_V2THE_I, 0.0f); // integral gain +PARAM_DEFINE_FLOAT(FWB_V2THE_D, 0.0f); // derivative gain +PARAM_DEFINE_FLOAT(FWB_V2THE_D_LP, 0.0f); // derivative low-pass +PARAM_DEFINE_FLOAT(FWB_V2THE_I_MAX, 0.0f); // integrator wind up guard +PARAM_DEFINE_FLOAT(FWB_THE_MIN, -0.5f); // the max commanded pitch angle +PARAM_DEFINE_FLOAT(FWB_THE_MAX, 0.5f); // the min commanded pitch angle // theta -> q -PARAM_DEFINE_FLOAT(FWB_THE2Q_P, 1.0f); +PARAM_DEFINE_FLOAT(FWB_THE2Q_P, 1.0f); // pitch angle to pitch-rate PID PARAM_DEFINE_FLOAT(FWB_THE2Q_I, 0.0f); PARAM_DEFINE_FLOAT(FWB_THE2Q_D, 0.0f); PARAM_DEFINE_FLOAT(FWB_THE2Q_D_LP, 0.0f); PARAM_DEFINE_FLOAT(FWB_THE2Q_I_MAX, 0.0f); // h -> thr -PARAM_DEFINE_FLOAT(FWB_H2THR_P, 0.01f); +PARAM_DEFINE_FLOAT(FWB_H2THR_P, 0.01f); // altitude to throttle PID PARAM_DEFINE_FLOAT(FWB_H2THR_I, 0.0f); PARAM_DEFINE_FLOAT(FWB_H2THR_D, 0.0f); PARAM_DEFINE_FLOAT(FWB_H2THR_D_LP, 0.0f); PARAM_DEFINE_FLOAT(FWB_H2THR_I_MAX, 0.0f); // crosstrack -PARAM_DEFINE_FLOAT(FWB_XT2YAW_MAX, 1.57f); // 90 deg -PARAM_DEFINE_FLOAT(FWB_XT2YAW, 0.002f); +PARAM_DEFINE_FLOAT(FWB_XT2YAW_MAX, 1.57f); // cross-track to yaw angle limit 90 deg +PARAM_DEFINE_FLOAT(FWB_XT2YAW, 0.005f); // cross-track to yaw angle gain // speed command -PARAM_DEFINE_FLOAT(FWB_V_MIN, 20.0f); -PARAM_DEFINE_FLOAT(FWB_V_CMD, 22.0f); -PARAM_DEFINE_FLOAT(FWB_V_MAX, 24.0f); +PARAM_DEFINE_FLOAT(FWB_V_MIN, 20.0f); // minimum commanded velocity +PARAM_DEFINE_FLOAT(FWB_V_CMD, 22.0f); // commanded velocity +PARAM_DEFINE_FLOAT(FWB_V_MAX, 24.0f); // maximum commanded velocity // trim -PARAM_DEFINE_FLOAT(FWB_TRIM_AIL, 0.0f); -PARAM_DEFINE_FLOAT(FWB_TRIM_ELV, 0.005f); -PARAM_DEFINE_FLOAT(FWB_TRIM_RDR, 0.0f); -PARAM_DEFINE_FLOAT(FWB_TRIM_THR, 0.81f); +PARAM_DEFINE_FLOAT(FWB_TRIM_AIL, 0.0f); // trim aileron, normalized (-1,1) +PARAM_DEFINE_FLOAT(FWB_TRIM_ELV, 0.005f); // trim elevator (-1,1) +PARAM_DEFINE_FLOAT(FWB_TRIM_RDR, 0.0f); // trim rudder (-1,1) +PARAM_DEFINE_FLOAT(FWB_TRIM_THR, 0.8f); // trim throttle (0,1) |