Description

Public Methods

CreateCalculationObjects	Creates the calculation objects for the selected coordinate system.
CreateIdealSecondaryCB	Constructs the idealized secondary for the three-body system.
CreatePropagator	Creates the propagator for the primary-secondary ER3BP formulation.
CreateRotatingCoordinateSystem	Creates the coordinate system for the RotatingSystemChoice selection.
DeleteCalculationObjects	Deletes the calculation objects for the selected coordinate system.
DeletePropagator	Deletes the propagator for the primary-secondary ER3BP formulation.
DeleteRotatingCoordinateSystem	Deletes the coordinate system for the RotatingSystemChoice selection.
ResetIdealSecondaryCB	Reset the idealized secondary for the three-body system.
UpdateIdealSecondaryCB	Update the idealized secondary for the three-body system.

Public Properties

AssociatedObjects	Get the list of associated objects.
CentralBodyName	Primary central body for the three-body system.
CharacteristicAcceleration	Get the characteristic acceleration computed from the primary and secondary bodies.
CharacteristicDistance	Get the characteristic distance computed from the primary and secondary bodies.
CharacteristicTime	Get the characteristic time computed from the primary and secondary bodies.
CharacteristicVelocity	Get the characteristic velocity computed from the primary and secondary bodies.
Eccentricity	Get the eccentricity at epoch to be used for constructing the orbit of the secondary body.
IdealSecondaryName	Name to be used for the idealized secondary.
IncludeSTM	Get whether or not the STM propagator function is included on the propagator.
InitialEpoch	Date and time for system construction.
MassParameter	Get the mass parameter computed from the primary and secondary bodies.
RotatingSystemChoice	Get the rotating coordinate system and associated calculation objects to interact with.
SecondaryBodyName	Secondary Body.
TrueAnomaly	True anomaly for initializing ideal secondary.

Interfaces

CoClasses that Implement IAgVADesignER3BPSetup