ContinuousThrustForceModelCreateVeThrustVector Method |
Creates a thrust
Vector where the thrust is computed from the
exhaustSpeed, and
massFlowRate pointing in the
thrustDirection
in the specified
burnAxes.
Namespace:
AGI.Foundation.Celestial
Assembly:
AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 24.3.420.0 (24.3.420.0)
Syntax public static Vector CreateVeThrustVector(
Scalar exhaustSpeed,
Scalar massFlowRate,
Axes burnAxes,
Vector thrustDirection
)
Public Shared Function CreateVeThrustVector (
exhaustSpeed As Scalar,
massFlowRate As Scalar,
burnAxes As Axes,
thrustDirection As Vector
) As Vector
public:
static Vector^ CreateVeThrustVector(
Scalar^ exhaustSpeed,
Scalar^ massFlowRate,
Axes^ burnAxes,
Vector^ thrustDirection
)
static member CreateVeThrustVector :
exhaustSpeed : Scalar *
massFlowRate : Scalar *
burnAxes : Axes *
thrustDirection : Vector -> Vector
Parameters
- exhaustSpeed
- Type: AGI.Foundation.GeometryScalar
The speed of the exhaust. - massFlowRate
- Type: AGI.Foundation.GeometryScalar
The fuel flow rate. - burnAxes
- Type: AGI.Foundation.GeometryAxes
The axes to compute the thrustDirection in. - thrustDirection
- Type: AGI.Foundation.GeometryVector
The direction of the thrust in the burnAxes.
Return Value
Type:
VectorA vector representing the thrust.
See Also