ER3BPFunc#
- class ansys.stk.core.stkobjects.astrogator.ER3BPFunc#
Bases:
IComponentInfo
,ICloneable
ER3BP Function.
Overview#
Get or set the secondary body which should be consistently defined with ER3BP model definitions. |
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Get the epoch from which the eccentricity value is reported from the secondary. |
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Get the true anomaly used for initializing ideal secondary. |
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Get the eccentricity at the reference epoch for the secondaryβs orbit. |
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Get the mass parameter computed from the primary and secondary bodies. |
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Get the characteristic distance computed from the primary and secondary bodies. |
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Get the characteristic time computed from the primary and secondary bodies. |
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Get the characteristic velocity computed from the primary and secondary bodies. |
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Get the characteristic acceleration computed from the primary and secondary bodies. |
Import detail#
from ansys.stk.core.stkobjects.astrogator import ER3BPFunc
Property detail#
- property ER3BPFunc.secondary_name: str#
Get or set the secondary body which should be consistently defined with ER3BP model definitions.
- property ER3BPFunc.ephemeris_epoch: Any#
Get the epoch from which the eccentricity value is reported from the secondary.
- property ER3BPFunc.eccentricity: float#
Get the eccentricity at the reference epoch for the secondaryβs orbit.
- property ER3BPFunc.mass_parameter: float#
Get the mass parameter computed from the primary and secondary bodies.
- property ER3BPFunc.characteristic_distance: float#
Get the characteristic distance computed from the primary and secondary bodies.
- property ER3BPFunc.characteristic_time: float#
Get the characteristic time computed from the primary and secondary bodies.