StateCalcCurvilinearRelativeMotion#

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

Bases: IComponentInfo, ICloneable

Curvilinear Relative Motion objects.

Overview#

Properties

`central_body_name`	Get or set the central body of the component.
`reference_ellipse`	Selection of the satellite orbit that is used as the reference ellipse.
`location_source`	Selection of the satellite whose location is being reported with respect to the reference ellipse.
`reference_selection`	Get or set the reference object selection.
`reference`	Get the reference object.
`element_type`	Choice of osculating or mean elements.
`sign_convention`	Get or set the sign of the angle when the relative position has a positive component along the orbit normal.

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

property StateCalcCurvilinearRelativeMotion.central_body_name: str#: Get or set the central body of the component.

property StateCalcCurvilinearRelativeMotion.reference_ellipse: CalculationObjectReferenceEllipse#: Selection of the satellite orbit that is used as the reference ellipse.

property StateCalcCurvilinearRelativeMotion.location_source: CalculationObjectLocationSource#: Selection of the satellite whose location is being reported with respect to the reference ellipse.

property StateCalcCurvilinearRelativeMotion.reference_selection: CalculationObjectReference#: Get or set the reference object selection.

property StateCalcCurvilinearRelativeMotion.reference: ILinkToObject#: Get the reference object.

property StateCalcCurvilinearRelativeMotion.element_type: CalculationObjectElement#: Choice of osculating or mean elements.

property StateCalcCurvilinearRelativeMotion.sign_convention: CalculationObjectAngleSign#: Get or set the sign of the angle when the relative position has a positive component along the orbit normal.