OrbitStateDelaunay#

class ansys.stk.core.stkobjects.OrbitStateDelaunay#

Bases: IOrbitState

Delaunay coordinate type, using a set of canonical action-angle variables, which are commonly used in general perturbation theories.

Overview#

Properties

`coordinate_system_type`	Get or set the coordinate system being used.
`coordinate_system`	Get the coordinate system and coordinate epoch.
`l_type`	Option for Delaunay L (default or L/SQRT(mu).
`l`	Value of L or L/SQRT(mu).
`h_type`	Option for Delaunay H (default or H/SQRT(mu).
`h`	Value of H or H/SQRT(mu).
`g_type`	Option for Delaunay G (default or G/SQRT(mu).
`g`	Value of G or G/SQRT(mu).
`supported_coordinate_system_types`	Return an array of supported coordinate system types.
`mean_anomaly`	Mean Anomaly (l). Uses Angle Dimension.
`argument_of_periapsis`	Argument of periapsis (g). Uses Angle Dimension.
`right_ascension_ascending_node`	RAAN (h). Uses Angle Dimension.
`state_epoch`	Smart epoch component allows the user to configure the state epoch explicitly or implicitly (using a pre-defined or custom time instant component).

from ansys.stk.core.stkobjects import OrbitStateDelaunay

property OrbitStateDelaunay.coordinate_system_type: CoordinateSystem#: Get or set the coordinate system being used.

property OrbitStateDelaunay.coordinate_system: OrbitStateCoordinateSystem#: Get the coordinate system and coordinate epoch.

property OrbitStateDelaunay.l_type: DelaunayLType#: Option for Delaunay L (default or L/SQRT(mu).

property OrbitStateDelaunay.l: IDelaunayActionVariable#: Value of L or L/SQRT(mu).

property OrbitStateDelaunay.h_type: DelaunayHType#: Option for Delaunay H (default or H/SQRT(mu).

property OrbitStateDelaunay.h: IDelaunayActionVariable#: Value of H or H/SQRT(mu).

property OrbitStateDelaunay.g_type: DelaunayGType#: Option for Delaunay G (default or G/SQRT(mu).

property OrbitStateDelaunay.g: IDelaunayActionVariable#: Value of G or G/SQRT(mu).

property OrbitStateDelaunay.supported_coordinate_system_types: list#: Return an array of supported coordinate system types.

property OrbitStateDelaunay.mean_anomaly: float#: Mean Anomaly (l). Uses Angle Dimension.

property OrbitStateDelaunay.argument_of_periapsis: float#: Argument of periapsis (g). Uses Angle Dimension.

property OrbitStateDelaunay.right_ascension_ascending_node: float#: RAAN (h). Uses Angle Dimension.

property OrbitStateDelaunay.state_epoch: ITimeToolInstantSmartEpoch#: Smart epoch component allows the user to configure the state epoch explicitly or implicitly (using a pre-defined or custom time instant component).