fix: pitch_flare_tweak

revert changes to flightmodel fine tune
headwindsim · Jan 9, 2025 · 80f59e2 · 80f59e2
1 parent 12024ec
commit 80f59e2
Showing 1 changed file with 11 additions and 11 deletions.
diff --git a/hdw-a339x/src/wasm/fbw_a330/src/model/PitchNormalLaw.cpp b/hdw-a339x/src/wasm/fbw_a330/src/model/PitchNormalLaw.cpp
@@ -1401,8 +1401,8 @@ void PitchNormalLaw::step(const real_T *rtu_In_time_dt, const real_T *rtu_In_nz_
     PitchNormalLaw_DWork.is_active_c2_PitchNormalLaw = 1U;
     PitchNormalLaw_DWork.is_c2_PitchNormalLaw = PitchNormalLaw_IN_Ground;
     rtb_in_flare = 0;
-    PitchNormalLaw_B.flare_Theta_c_deg = -2.0;
-    PitchNormalLaw_B.flare_Theta_c_rate_deg_s = -1000.0;
+    PitchNormalLaw_B.flare_Theta_c_deg = 0.0;
+    PitchNormalLaw_B.flare_Theta_c_rate_deg_s = 0.0;
   } else {
     switch (PitchNormalLaw_DWork.is_c2_PitchNormalLaw) {
      case PitchNormalLaw_IN_Flare_Active_Armed:
@@ -1415,7 +1415,7 @@ void PitchNormalLaw::step(const real_T *rtu_In_time_dt, const real_T *rtu_In_nz_
       if ((*rtu_In_H_radio_ft <= 30.0) || (rtb_Switch_f == 1.0)) {
         PitchNormalLaw_DWork.is_c2_PitchNormalLaw = PitchNormalLaw_IN_Flare_Active_Reduce;
         rtb_in_flare = 1;
-        PitchNormalLaw_B.flare_Theta_c_deg = -2.0;
+        PitchNormalLaw_B.flare_Theta_c_deg = 0.0;
       } else if ((*rtu_In_in_flight == 1.0) && (*rtu_In_H_radio_ft > 50.0) && (rtb_ManualSwitch == 0.0)) {
         PitchNormalLaw_DWork.is_c2_PitchNormalLaw = PitchNormalLaw_IN_Flight;
         rtb_in_flare = 0;
@@ -1428,20 +1428,20 @@ void PitchNormalLaw::step(const real_T *rtu_In_time_dt, const real_T *rtu_In_nz_
       if (*rtu_In_in_flight == 0.0) {
         PitchNormalLaw_DWork.is_c2_PitchNormalLaw = PitchNormalLaw_IN_Ground;
         rtb_in_flare = 0;
-        PitchNormalLaw_B.flare_Theta_c_deg = -2.0;
-        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = -1000.0;
+        PitchNormalLaw_B.flare_Theta_c_deg = 0.0;
+        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = 0.0;
       } else if ((*rtu_In_in_flight == 1.0) && (*rtu_In_H_radio_ft > 50.0) && (rtb_ManualSwitch == 0.0)) {
         PitchNormalLaw_DWork.is_c2_PitchNormalLaw = PitchNormalLaw_IN_Flight;
         rtb_in_flare = 0;
       } else {
         rtb_in_flare = 1;
-        PitchNormalLaw_B.flare_Theta_c_deg = -2.0;
+        PitchNormalLaw_B.flare_Theta_c_deg = 0.0;
       }
       break;
 
      case PitchNormalLaw_IN_Flare_Prepare:
       if ((*rtu_In_H_radio_ft <= 50.0) || (rtb_ManualSwitch == 1.0)) {
-        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = -(std::fmax(-2.0, rtb_Y_j) + 2.0) / 8.0;
+        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = -1000.0;
         PitchNormalLaw_DWork.is_c2_PitchNormalLaw = PitchNormalLaw_IN_Flare_Active_Armed;
         rtb_in_flare = 1;
       } else if ((*rtu_In_in_flight == 1.0) && (*rtu_In_H_radio_ft > 50.0) && (rtb_ManualSwitch == 0.0)) {
@@ -1454,8 +1454,8 @@ void PitchNormalLaw::step(const real_T *rtu_In_time_dt, const real_T *rtu_In_nz_
 
      case PitchNormalLaw_IN_Flight:
       if ((*rtu_In_H_radio_ft <= 50.0) || (rtb_ManualSwitch == 1.0)) {
-        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = -1000.0;
-        PitchNormalLaw_B.flare_Theta_c_deg = rtb_Y_j;
+        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = 0.0;
+        PitchNormalLaw_B.flare_Theta_c_deg = rtb_Y_cf;
         PitchNormalLaw_DWork.is_c2_PitchNormalLaw = PitchNormalLaw_IN_Flare_Prepare;
         rtb_in_flare = 0;
       } else {
@@ -1469,8 +1469,8 @@ void PitchNormalLaw::step(const real_T *rtu_In_time_dt, const real_T *rtu_In_nz_
         rtb_in_flare = 0;
       } else {
         rtb_in_flare = 0;
-        PitchNormalLaw_B.flare_Theta_c_deg = -2.0;
-        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = -1000.0;
+        PitchNormalLaw_B.flare_Theta_c_deg = 0.0;
+        PitchNormalLaw_B.flare_Theta_c_rate_deg_s = 0.0;
       }
       break;
     }