Create aerodynamics_and_heat_shield_simulator.csharp

core/aerospace/aerodynamics_and_heat_shield_simulator.csharp

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+using System;
+using System.Collections.Generic;
+
+public class AerodynamicsAndHeatShieldSimulator {
+    private List<Spacecraft> spacecraftList;
+    private List<AtmosphericCondition> atmosphericConditionList;
+
+    public AerodynamicsAndHeatShieldSimulator() {
+        spacecraftList = new List<Spacecraft>();
+        atmosphericConditionList = new List<AtmosphericCondition>();
+    }
+
+    public void simulateAerodynamicsAndHeatShield(Spacecraft spacecraft, AtmosphericCondition atmosphericCondition) {
+        // Calculate aerodynamic forces and moments
+        double liftForce = calculateLiftForce(spacecraft, atmosphericCondition);
+        double dragForce = calculateDragForce(spacecraft, atmosphericCondition);
+        double pitchingMoment = calculatePitchingMoment(spacecraft, atmosphericCondition);
+
+        // Calculate heat shield temperature
+        double heatShieldTemperature = calculateHeatShieldTemperature(spacecraft, atmosphericCondition);
+
+        // Update spacecraft position and velocity
+        spacecraft.updatePositionAndVelocity(liftForce, dragForce, pitchingMoment);
+    }
+
+    private double calculateLiftForce(Spacecraft spacecraft, AtmosphericCondition atmosphericCondition) {
+        // Calculate lift force using lift equation
+        return 0.5 * atmosphericCondition.getAirDensity() * spacecraft.getLiftCoefficient() * spacecraft.getVelocity() * spacecraft.getVelocity();
+    }
+
+    private double calculateDragForce(Spacecraft spacecraft, AtmosphericCondition atmosphericCondition) {
+        // Calculate drag force using drag equation
+        return 0.5 * atmosphericCondition.getAirDensity() * spacecraft.getDragCoefficient() * spacecraft.getVelocity() * spacecraft.getVelocity();
+    }
+
+    private double calculatePitchingMoment(Spacecraft spacecraft, AtmosphericCondition atmosphericCondition) {
+        // Calculate pitching moment using pitching moment equation
+        return 0.5 * atmosphericCondition.getAirDensity() * spacecraft.getPitchingMomentCoefficient() * spacecraft.getVelocity() * spacecraft.getVelocity();
+    }
+
+    private double calculateHeatShieldTemperature(Spacecraft spacecraft, AtmosphericCondition atmosphericCondition) {
+        // Calculate heat shield temperature using heat shield equation
+        return atmosphericCondition.getTemperature() + spacecraft.getHeatShieldCoefficient() * spacecraft.getVelocity() * spacecraft.getVelocity();
+    }
+}