CR3BPFunction#

class ansys.stk.core.stkobjects.astrogator.CR3BPFunction#

Bases: IComponentInfo, ICloneable

CR3BP Function.

Overview#

secondary_name

Get or set the secondary body which should be consistently defined with CR3BP model definitions.

ephemeris_epoch

Get the epoch from which the eccentricity value is reported from the secondary.

eccentricity

Get the eccentricity at the reference epoch for the secondary’s orbit.

mass_parameter

Get the mass parameter computed from the primary and secondary bodies.

characteristic_distance

Get the characteristic distance computed from the primary and secondary bodies.

characteristic_time

Get the characteristic time computed from the primary and secondary bodies.

characteristic_velocity

Get the characteristic velocity computed from the primary and secondary bodies.

characteristic_acceleration

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 secondary’s 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.

property CR3BPFunction.characteristic_velocity: float#

Get the characteristic velocity computed from the primary and secondary bodies.

property CR3BPFunction.characteristic_acceleration: float#

Get the characteristic acceleration computed from the primary and secondary bodies.