StkEphemerisFileCovarianceTimePosVel Class

A class that holds the covariance data in the ephemeris file when the ephemeris file is in the "CovarianceTimePosVel" format.

Inheritance Hierarchy

SystemObject
AGI.Foundation.StkStkEphemerisFileCovariance
AGI.Foundation.StkStkEphemerisFileCovarianceTimePosVel

Namespace: AGI.Foundation.Stk
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.1.418.0 (24.1.418.0)

Syntax

public class CovarianceTimePosVel : StkEphemerisFileCovariance

Public Class CovarianceTimePosVel
	Inherits StkEphemerisFileCovariance

public ref class CovarianceTimePosVel : public StkEphemerisFileCovariance

type CovarianceTimePosVel =  
    class
        inherit StkEphemerisFileCovariance
    end

The StkEphemerisFileCovarianceTimePosVel type exposes the following members.

Constructors

	Name	Description
	StkEphemerisFileCovarianceTimePosVel	Initializes a new instance of the StkEphemerisFileCovarianceTimePosVel class

Properties

	Name	Description
	Blender	Gets or sets a two-body covariance blender consistent with this covariance data.
	CoordinateAxes	Gets the axes in which this covariance data is observed. (Inherited from StkEphemerisFileCovariance.)
	CovarianceData	Gets or sets the covariance data.
	DistanceUnit	Gets the distance unit of the ephemeris and covariance information. (Overrides StkEphemerisFileCovarianceDistanceUnit.)
	Interpolator	Gets or sets the interpolator to use to interpolate this covariance data. (Overrides StkEphemerisFileCovarianceInterpolator.)
	Name	Gets the name of this covariance format. (Overrides StkEphemerisFileCovarianceName.)
	SegmentBoundaryTimes	Gets the segment boundary times of the data. (Overrides StkEphemerisFileCovarianceSegmentBoundaryTimes.)
	Times	Gets the times of the data points. (Overrides StkEphemerisFileCovarianceTimes.)

Methods

	Name	Description
	CreateBlender(StkEphemerisFileEphemerisTimePosVel)	Creates a two-body covariance blender from the orbit states ephemeris and the covariance data. Also, sets the Blender property to the created value. The InertialPropagationFrame is set to the inertial frame of the instance of EarthCentralBody in the CentralBodiesFacet of the CalculationContext. The GravitationalParameter is set to that of the WorldGeodeticSystem1984.
	CreateBlender(StkEphemerisFileEphemerisTimePosVel, ReferenceFrame, NullableDouble)	Creates a two-body covariance blender from the orbit states ephemeris and the covariance data. Also, sets the Blender property to the created value.
	Equals	Determines whether the specified object is equal to the current object. (Inherited from Object.)
	Finalize	Allows an object to try to free resources and perform other cleanup operations before it is reclaimed by garbage collection. (Inherited from Object.)
	GetHashCode	Serves as the default hash function. (Inherited from Object.)
	GetType	Gets the Type of the current instance. (Inherited from Object.)
	MemberwiseClone	Creates a shallow copy of the current Object. (Inherited from Object.)
	ToString	Returns a string that represents the current object. (Inherited from Object.)

StkEphemerisFileAddLanguageSpecificTextSet("LST5EFAC962_0?cpp=::|nu=.");CovarianceTimePosVel Class