StateCalcRelativeInclination

class ansys.stk.core.stkobjects.astrogator.StateCalcRelativeInclination

Bases: IComponentInfo, ICloneable

Relative Inclination Angle objects.

Overview

Properties

central_body_name	Get or set the central body of the component.
satellite_orbit_normal_type	Choice of osculating or mean elements for describing the orbit plane.
reference_satellite_orbit_normal_type	Choice of osculating or mean elements for describing the orbit plane.
reference_selection	Get or set the reference object selection.
reference	Get the reference object.

Import detail

from ansys.stk.core.stkobjects.astrogator import StateCalcRelativeInclination

Property detail

property StateCalcRelativeInclination.central_body_name: str

Get or set the central body of the component.

property StateCalcRelativeInclination.satellite_orbit_normal_type: CalculationObjectElement

Choice of osculating or mean elements for describing the orbit plane.

property StateCalcRelativeInclination.reference_satellite_orbit_normal_type: CalculationObjectElement

Choice of osculating or mean elements for describing the orbit plane.

property StateCalcRelativeInclination.reference_selection: CalculationObjectReference

Get or set the reference object selection.

property StateCalcRelativeInclination.reference: ILinkToObject

Get the reference object.