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C# Class SpaceSim.Spacecrafts.SpaceCraftBase

Datei anzeigen Open project: zlynn1990/SpaceSim Class Usage Examples

Protected Properties

Property	Type	Description
EntryFlame	ReEntryFlame
IspMultiplier	double
MachNumber	double
MissionName	string
StageOffset	VectorMath.DVector2
Texture	System.Drawing.Bitmap

Public Methods

Method	Description
AddChild ( ISpaceCraft child ) : void
ComputeBoundingBox ( ) : RectangleD
DeployFairing ( ) : void	Deploys the fairing.
DeployGridFins ( ) : void	Deploys the grid fins.
DeployLandingLegs ( ) : void	Deploys the landing legs.
FixedUpdate ( SpaceSim.Physics.TimeStep timeStep ) : void
GetAlpha ( ) : double
GetBaseCd ( double baseCd ) : double
GetDownrangeDistance ( DVector2 pointOfReference ) : double	Gets the down range distance along the equator of the parent planet.
GetRelativeAcceleration ( ) : DVector2
GetRelativeAltitude ( ) : double	Gets the relative altitude of the spacecraft from it's parent's surface.
GetRelativePitch ( ) : double
GetRelativeVelocity ( ) : DVector2	Gets the relative velocity of the spacecraft. If the space craft is within the parent's atmosphere than the rotation of the planet is taken in account. Otherwise its a simple difference of velocities.
InitializeController ( EventManager eventManager ) : void
OffsetPitch ( double offset ) : void
OffsetRelativePitch ( double offset ) : void
OffsetRoll ( double offset ) : void
OffsetYaw ( double offset ) : void
RemoveChild ( ISpaceCraft child ) : void
RenderGdi ( Graphics graphics, RectangleD cameraBounds ) : void	Renders the space craft at it's correct scale and rotation according to the camera. The engines are rendered first and then the space craft body.
ResetAccelerations ( ) : void
ResolveAtmopsherics ( IMassiveBody body ) : void
ResolveGravitation ( IPhysicsBody other ) : void
SetParent ( ISpaceCraft craft ) : void
SetPitch ( double pitch ) : void
SetRelativePitch ( double pitch ) : void
SetRoll ( double roll ) : void
SetThrottle ( double throttle, int engineIds = null ) : void
SetYaw ( double yaw ) : void
Stage ( ) : void	Stages the spacecraft according to its mounted angle by applying a normal force.
ToString ( ) : string
ToggleDisplayVectors ( ) : void
Update ( double dt ) : void	Updates the spacecraft and it's children.
UpdateAnimations ( SpaceSim.Physics.TimeStep timeStep ) : void
UpdateChildren ( DVector2 position, DVector2 velocity ) : void
UpdateController ( double dt ) : void
Visibility ( RectangleD cameraBounds ) : double

Protected Methods

Method	Description
RenderAbove ( Graphics graphics, RectangleD cameraBounds ) : void
RenderBelow ( Graphics graphics, RectangleD cameraBounds ) : void
RenderShip ( Graphics graphics, RectangleD cameraBounds, RectangleF screenBounds ) : void
SpaceCraftBase ( string craftDirectory, DVector2 position, DVector2 velocity, double payloadMass, double propellantMass, string texturePath, ReEntryFlame entryFlame = null ) : System

Private Methods

Method	Description
GetChildDragCoefficient ( List children, double totalDragCoefficient ) : double
GetChildFormDragArea ( List children, double totalFormDragArea ) : double
GetChildLiftArea ( List children, double totalLiftArea ) : double
GetMaxChildLiftCoefficient ( List children, double totalLiftCoefficient ) : double
TotalFormDragArea ( ) : double	Recursively finds the total drag area of all surfaces exposed to air in the spacecraft.
TotalFormDragCoefficient ( ) : double	Recursively finds the total drag of all surfaces exposed to air in the spacecraft.
TotalLiftArea ( ) : double	Recursively finds the total lift area of all surfaces exposed to air in the spacecraft.
TotalLiftCoefficient ( ) : double	Recursively finds the total lift of all surfaces exposed to air in the spacecraft.
TotalSkinFrictionArea ( ) : double	Recursively finds the total drag area of all surfaces exposed to air in the spacecraft.
TotalSkinFrictionCoefficient ( ) : double	Recursively finds the total skin friction due to all surfaces exposed to air in the spacecraft.
UpdateEngines ( double dt ) : void	Recursively updates the engines in the spacecraft and updates propellant mass.

Method Details

Property Details