PropagatorSimpleAscent

class ansys.stk.core.stkobjects.PropagatorSimpleAscent

Bases: IPropagator

Class defining the simple ascent propagator for a launch vehicle.

Overview

Methods

propagate

Propagates the launch vehicle’s path using the specified time interval.

Properties

step	Step size. Uses Time Dimension.
initial_state	Get the initial state.
ephemeris_interval	Get the propagator’s ephemeris interval.

Import detail

from ansys.stk.core.stkobjects import PropagatorSimpleAscent

Property detail

property PropagatorSimpleAscent.step: float

Step size. Uses Time Dimension.

property PropagatorSimpleAscent.initial_state: LaunchVehicleInitialState

Get the initial state.

property PropagatorSimpleAscent.ephemeris_interval: ITimeToolTimeIntervalSmartInterval

Get the propagator’s ephemeris interval.

Method detail

PropagatorSimpleAscent.propagate(self) → None

Propagates the launch vehicle’s path using the specified time interval.

Returns:

None