Properties for the ER3BP propagator function.
![]() | Get the characteristic acceleration computed from the primary and secondary bodies. |
![]() | Get the characteristic distance computed from the primary and secondary bodies. |
![]() | Get the characteristic time computed from the primary and secondary bodies. |
![]() | Get the characteristic velocity computed from the primary and secondary bodies. |
![]() | Get the eccentricity at the reference epoch for the secondary's orbit. |
![]() | Get the epoch from which the eccentricity value is reported from the secondary. |
![]() | Get the mass parameter computed from the primary and secondary bodies. |
![]() | Gets or sets the secondary body which should be consistently defined with ER3BP model definitions. |
![]() | Get the true anomaly used for initializing ideal secondary. |
Implemented Interface |
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IAgComponentInfo |
IAgCloneable |
Name |
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AgVAER3BPFunc |