feat(ap): Tuning of A380X Autoland (flybywiresim#8999)

feat(ap): Tuning of A380X Autoland flybywiresim#8999

fbw-a380x/src/wasm/fbw_a380/build.sh

@@ -126,11 +126,9 @@ clang++ \
   "${DIR}/src/model/FacComputer_data.cpp" \
   "${DIR}/src/model/FacComputer.cpp" \
   "${DIR}/src/model/look1_binlxpw.cpp" \
-  "${DIR}/src/model/look2_binlcpw.cpp" \
   "${DIR}/src/model/look2_binlxpw.cpp" \
   "${DIR}/src/model/look2_pbinlxpw.cpp" \
-  "${DIR}/src/model/mod_mvZvttxs.cpp" \
-  "${DIR}/src/model/mod_2RcCQkwc.cpp" \
+  "${DIR}/src/model/mod_OlzklkXq.cpp" \
   "${DIR}/src/model/MultiWordIor.cpp" \
   "${DIR}/src/model/rt_modd.cpp" \
   "${DIR}/src/model/rt_remd.cpp" \

fbw-a380x/src/wasm/fbw_a380/src/FlyByWireInterface.cpp

@@ -1858,7 +1858,7 @@ bool FlyByWireInterface::updateFac(double sampleTime, int facIndex) {
   idFacCenterOfGravity[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].center_of_gravity_pos_percent));
   idFacSideslipTarget[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].sideslip_target_deg));
   idFacSlatAngle[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].fac_slat_angle_deg));
-  idFacFlapAngle[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].fac_flap_angle));
+  idFacFlapAngle[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].fac_flap_angle_deg));
   idFacDiscreteWord2[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].discrete_word_2));
   idFacRudderTravelLimitCommand[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].rudder_travel_limit_command_deg));
   idFacDeltaRYawDamperVoted[facIndex]->set(Arinc429Utils::toSimVar(facsBusOutputs[facIndex].delta_r_yaw_damper_deg));
@@ -2121,8 +2121,10 @@ bool FlyByWireInterface::updateAutopilotStateMachine(double sampleTime) {
     autopilotStateMachineInput.in.data.cruise_altitude = idFmgcCruiseAltitude->get();
     autopilotStateMachineInput.in.data.throttle_lever_1_pos = thrustLeverAngle_1->get();
     autopilotStateMachineInput.in.data.throttle_lever_2_pos = thrustLeverAngle_2->get();
-    autopilotStateMachineInput.in.data.gear_strut_compression_1 = simData.gear_animation_pos_1;
-    autopilotStateMachineInput.in.data.gear_strut_compression_2 = simData.gear_animation_pos_2;
+    autopilotStateMachineInput.in.data.gear_strut_compression_1 =
+        std::max(simData.contact_point_compression_1 * 0.5 + 0.5, simData.contact_point_compression_3 * 0.5 + 0.5);
+    autopilotStateMachineInput.in.data.gear_strut_compression_2 =
+        std::max(simData.contact_point_compression_2 * 0.5 + 0.5, simData.contact_point_compression_4 * 0.5 + 0.5);
     autopilotStateMachineInput.in.data.zeta_pos = simData.zeta_pos;
     autopilotStateMachineInput.in.data.flaps_handle_index = flapsHandleIndexFlapConf->get();
     autopilotStateMachineInput.in.data.is_engine_operative_1 = simData.engine_combustion_1;
@@ -2471,8 +2473,10 @@ bool FlyByWireInterface::updateAutopilotLaws(double sampleTime) {
     autopilotLawsInput.in.data.acceleration_altitude_go_around_engine_out = fmAccelerationAltitudeGoAroundEngineOut->valueOr(0);
     autopilotLawsInput.in.data.throttle_lever_1_pos = thrustLeverAngle_1->get();
     autopilotLawsInput.in.data.throttle_lever_2_pos = thrustLeverAngle_2->get();
-    autopilotLawsInput.in.data.gear_strut_compression_1 = simData.gear_animation_pos_1;
-    autopilotLawsInput.in.data.gear_strut_compression_2 = simData.gear_animation_pos_2;
+    autopilotLawsInput.in.data.gear_strut_compression_1 =
+        std::max(simData.contact_point_compression_1 * 0.5 + 0.5, simData.contact_point_compression_3 * 0.5 + 0.5);
+    autopilotLawsInput.in.data.gear_strut_compression_2 =
+        std::max(simData.contact_point_compression_2 * 0.5 + 0.5, simData.contact_point_compression_4 * 0.5 + 0.5);
     autopilotLawsInput.in.data.zeta_pos = simData.zeta_pos;
     autopilotLawsInput.in.data.flaps_handle_index = flapsHandleIndexFlapConf->get();
     autopilotLawsInput.in.data.is_engine_operative_1 = simData.engine_combustion_1;
@@ -2686,8 +2690,10 @@ bool FlyByWireInterface::updateAutothrust(double sampleTime) {
     autoThrustInput.in.data.bx_m_s2 = simData.bx_m_s2;
     autoThrustInput.in.data.by_m_s2 = simData.by_m_s2;
     autoThrustInput.in.data.bz_m_s2 = simData.bz_m_s2;
-    autoThrustInput.in.data.gear_strut_compression_1 = simData.gear_animation_pos_1;
-    autoThrustInput.in.data.gear_strut_compression_2 = simData.gear_animation_pos_2;
+    autoThrustInput.in.data.gear_strut_compression_1 =
+        std::max(simData.contact_point_compression_1 * 0.5 + 0.5, simData.contact_point_compression_3 * 0.5 + 0.5);
+    autoThrustInput.in.data.gear_strut_compression_2 =
+        std::max(simData.contact_point_compression_2 * 0.5 + 0.5, simData.contact_point_compression_4 * 0.5 + 0.5);
     autoThrustInput.in.data.flap_handle_index = flapsHandleIndexFlapConf->get();
     autoThrustInput.in.data.is_engine_operative_1 = simData.engine_combustion_1;
     autoThrustInput.in.data.is_engine_operative_2 = simData.engine_combustion_2;

fbw-a380x/src/wasm/fbw_a380/src/fac/Fac.cpp

@@ -99,7 +99,7 @@ base_fac_bus Fac::getBusOutputs() {
     output.center_of_gravity_pos_percent.SSM = Arinc429SignStatus::FailureWarning;
     output.sideslip_target_deg.SSM = Arinc429SignStatus::FailureWarning;
     output.fac_slat_angle_deg.SSM = Arinc429SignStatus::FailureWarning;
-    output.fac_flap_angle.SSM = Arinc429SignStatus::FailureWarning;
+    output.fac_flap_angle_deg.SSM = Arinc429SignStatus::FailureWarning;
     output.rudder_travel_limit_command_deg.SSM = Arinc429SignStatus::FailureWarning;
     output.delta_r_yaw_damper_deg.SSM = Arinc429SignStatus::FailureWarning;
     output.estimated_sideslip_deg.SSM = Arinc429SignStatus::FailureWarning;

fbw-a380x/src/wasm/fbw_a380/src/interface/SimConnectData.h

@@ -140,6 +140,11 @@ struct SimData {
   double wheelRpmRightBlg;
   double wheelRpmLeftWlg;
   double wheelRpmRightWlg;
+  double contact_point_compression_0;
+  double contact_point_compression_1;
+  double contact_point_compression_2;
+  double contact_point_compression_3;
+  double contact_point_compression_4;
 };
 
 struct SimInput {

fbw-a380x/src/wasm/fbw_a380/src/interface/SimConnectInterface.cpp

@@ -272,6 +272,11 @@ bool SimConnectInterface::prepareSimDataSimConnectDataDefinitions() {
   result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "WHEEL RPM:2", "RPM");
   result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "WHEEL RPM:3", "RPM");
   result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "WHEEL RPM:4", "RPM");
+  result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "CONTACT POINT COMPRESSION", "PERCENT");
+  result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "CONTACT POINT COMPRESSION:1", "PERCENT");
+  result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "CONTACT POINT COMPRESSION:2", "PERCENT");
+  result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "CONTACT POINT COMPRESSION:3", "PERCENT");
+  result &= addDataDefinition(hSimConnect, 0, SIMCONNECT_DATATYPE_FLOAT64, "CONTACT POINT COMPRESSION:4", "PERCENT");
 
   return result;
 }

fbw-a380x/src/wasm/fbw_a380/src/model/A380LateralDirectLaw.h

@@ -1,5 +1,5 @@
-#ifndef RTW_HEADER_A380LateralDirectLaw_h_
-#define RTW_HEADER_A380LateralDirectLaw_h_
+#ifndef A380LateralDirectLaw_h_
+#define A380LateralDirectLaw_h_
 #include "rtwtypes.h"
 #include "A380LateralDirectLaw_types.h"
 #include <cstring>

fbw-a380x/src/wasm/fbw_a380/src/model/A380LateralDirectLaw_private.h

@@ -1,5 +1,5 @@
-#ifndef RTW_HEADER_A380LateralDirectLaw_private_h_
-#define RTW_HEADER_A380LateralDirectLaw_private_h_
+#ifndef A380LateralDirectLaw_private_h_
+#define A380LateralDirectLaw_private_h_
 #include "rtwtypes.h"
 #include "A380LateralDirectLaw_types.h"
 #endif

fbw-a380x/src/wasm/fbw_a380/src/model/A380LateralDirectLaw_types.h

@@ -1,4 +1,4 @@
-#ifndef RTW_HEADER_A380LateralDirectLaw_types_h_
-#define RTW_HEADER_A380LateralDirectLaw_types_h_
+#ifndef A380LateralDirectLaw_types_h_
+#define A380LateralDirectLaw_types_h_
 #endif