Covariance6By6TwoBodyBlender Constructor (DateMotionCollectionCartesian, DateMotionCollectionMatrix, ReferenceFrame, Axes, ReferenceFrame, Double) |
Initializes a new instance.
Namespace:
AGI.Foundation.NumericalMethods
Assembly:
AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)
Syntax public Covariance6By6TwoBodyBlender(
DateMotionCollection<Cartesian> orbitStates,
DateMotionCollection<Matrix> covarianceData,
ReferenceFrame orbitStatesFrame,
Axes covarianceAxes,
ReferenceFrame inertialPropagationFrame,
double gravitationalParameter
)
Public Sub New (
orbitStates As DateMotionCollection(Of Cartesian),
covarianceData As DateMotionCollection(Of Matrix),
orbitStatesFrame As ReferenceFrame,
covarianceAxes As Axes,
inertialPropagationFrame As ReferenceFrame,
gravitationalParameter As Double
)
public:
Covariance6By6TwoBodyBlender(
DateMotionCollection<Cartesian>^ orbitStates,
DateMotionCollection<Matrix^>^ covarianceData,
ReferenceFrame^ orbitStatesFrame,
Axes^ covarianceAxes,
ReferenceFrame^ inertialPropagationFrame,
double gravitationalParameter
)
new :
orbitStates : DateMotionCollection<Cartesian> *
covarianceData : DateMotionCollection<Matrix> *
orbitStatesFrame : ReferenceFrame *
covarianceAxes : Axes *
inertialPropagationFrame : ReferenceFrame *
gravitationalParameter : float -> Covariance6By6TwoBodyBlender
Parameters
- orbitStates
- Type: AGI.FoundationDateMotionCollectionCartesian
The position and velocity vectors of the spacecraft at the same times
as the covarianceData. - covarianceData
- Type: AGI.FoundationDateMotionCollectionMatrix
The covariance data that is used for blending. - orbitStatesFrame
- Type: AGI.Foundation.GeometryReferenceFrame
The native reference frame of the orbitStates. - covarianceAxes
- Type: AGI.Foundation.GeometryAxes
The native axes of the covarianceData. - inertialPropagationFrame
- Type: AGI.Foundation.GeometryReferenceFrame
The inertial propagation frame that is used to propagate the orbitStates
and the covarianceData. - gravitationalParameter
- Type: SystemDouble
The gravitational parameter of the central body that the spacecraft is orbiting.
See Also