TwoBodyPropagator Constructor (JulianDate, ReferenceFrame, EquinoctialElements) |
Initializes a new instance.
Namespace:
AGI.Foundation.Propagators
Assembly:
AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)
Syntaxpublic TwoBodyPropagator(
JulianDate orbitEpoch,
ReferenceFrame referenceFrame,
EquinoctialElements elements
)
Public Sub New (
orbitEpoch As JulianDate,
referenceFrame As ReferenceFrame,
elements As EquinoctialElements
)
public:
TwoBodyPropagator(
JulianDate orbitEpoch,
ReferenceFrame^ referenceFrame,
EquinoctialElements^ elements
)
new :
orbitEpoch : JulianDate *
referenceFrame : ReferenceFrame *
elements : EquinoctialElements -> TwoBodyPropagator
Parameters
- orbitEpoch
- Type: AGI.Foundation.Time.JulianDate
The Julian date at which the initial conditions are defined. - referenceFrame
- Type: AGI.Foundation.Geometry.ReferenceFrame
The reference frame in which the elements are defined.
Generally this should be the InertialFrame of the central body
around which you are propagating. See the Remarks section for more information.
- elements
- Type: AGI.Foundation.Coordinates.EquinoctialElements
The elements from which to propagate.
Remarks
See Also