CR3BPFunction#
- class ansys.stk.core.stkobjects.astrogator.CR3BPFunction#
Bases:
IComponentInfo
,ICloneable
CR3BP Function.
Overview#
Get or set the secondary body which should be consistently defined with CR3BP model definitions. |
|
Get the epoch from which the eccentricity value is reported from the secondary. |
|
Get the eccentricity at the reference epoch for the secondaryβs orbit. |
|
Get the mass parameter 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 characteristic acceleration computed from the primary and secondary bodies. |
Import detail#
from ansys.stk.core.stkobjects.astrogator import CR3BPFunction
Property detail#
- property CR3BPFunction.secondary_name: str#
Get or set the secondary body which should be consistently defined with CR3BP model definitions.
- property CR3BPFunction.ephemeris_epoch: Any#
Get the epoch from which the eccentricity value is reported from the secondary.
- property CR3BPFunction.eccentricity: float#
Get the eccentricity at the reference epoch for the secondaryβs orbit.
- property CR3BPFunction.mass_parameter: float#
Get the mass parameter computed from the primary and secondary bodies.
- property CR3BPFunction.characteristic_distance: float#
Get the characteristic distance computed from the primary and secondary bodies.
- property CR3BPFunction.characteristic_time: float#
Get the characteristic time computed from the primary and secondary bodies.