public Capsule(InitialConditionsDTO initConditions)
: base(initConditions)
{
CrossSectionalArea = Math.PI * Math.Pow(Radius, 2);
CalculateBallisticCoeff();
CalculateLdCoeff();
}
public SpaceVehicle(InitialConditionsDTO initConditions)
{
Mass = initConditions.Mass;
_initVelocity = initConditions.Velocity;
Velocity = initConditions.Velocity;
Radius = initConditions.Radius;
_initHeight = initConditions.Height;
Height = initConditions.Height;
AngleOfAttack = initConditions.AngleOfAttack;
_initAngleBelowHorizontal = initConditions.AngleBelowHorizontal;
AngleBelowHorizontal = initConditions.AngleBelowHorizontal;
}
public void Init()
{
Simulation = new Core.Simulation();
var conditions = new InitialConditionsDTO()
{
AngleBelowHorizontal = 6.93,
AngleOfAttack = 20,
Height = 80000,
Mass = 78000,
Radius = 6.6,
Velocity = 8000
};
Simulation.SetupEnvironment(5, conditions, Core.Simulation.VehicleType.SpaceShuttle);
}
public void TestMass()
{
int mass = Simulation.SpaceVehicle.Mass;
while (Simulation.SpaceVehicle.Mass > 10000)
{
mass -= 1000;
var conditions = new InitialConditionsDTO()
{
AngleBelowHorizontal = 6.93,
AngleOfAttack = 20,
Height = 80000,
Mass = mass,
Radius = 6.6,
Velocity = 8000
};
Simulation.SetupEnvironment(5, conditions, Core.Simulation.VehicleType.SpaceShuttle);
RunSimulation();
}
}
public void Init(double timeFrame, InitialConditionsDTO initConditions, Core.Simulation.VehicleType vehicleType)
{
_simulation = new Core.Simulation();
_simulation.SetupEnvironment(timeFrame, initConditions, vehicleType);
}
