PropagatorLOP#

class ansys.stk.core.stkobjects.PropagatorLOP#

Bases: IPropagator

Class defining the Long-term Orbit Predictor (LOP).

Overview#

propagate

Propagates the satellite’s path using the specified time interval.

step

Step size. Uses Time Dimension.

initial_state

Get the initial state.

force_model

Get the force model parameters.

ephemeris_interval

Get the propagator’s ephemeris interval.

display_coordinate_type

The propagator’s display coordinate type.

Import detail#

from ansys.stk.core.stkobjects import PropagatorLOP

Property detail#

property PropagatorLOP.step: float#

Step size. Uses Time Dimension.

property PropagatorLOP.initial_state: VehicleInitialState#

Get the initial state.

property PropagatorLOP.force_model: VehicleLOPForceModel#

Get the force model parameters.

property PropagatorLOP.ephemeris_interval: ITimeToolTimeIntervalSmartInterval#

Get the propagator’s ephemeris interval.

property PropagatorLOP.display_coordinate_type: PropagatorDisplayCoordinateType#

The propagator’s display coordinate type.

Method detail#

PropagatorLOP.propagate(self) None#

Propagates the satellite’s path using the specified time interval.

Returns:

None