ManeuverFinitePropagator#

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

Bases: IRuntimeTypeInfoProvider

Propagation for a finite maneuver.

Overview#

Properties

`propagator_name`	Get or set the propagator.
`stopping_conditions`	Get the stopping conditions list.
`min_propagation_time`	Minimum Propagation Time - the minimum time that must elapse from the beginning of the segment until Astrogator will begin checking stopping conditions for satisfaction. Uses Time Dimension.
`max_propagation_time`	Maximum Propagation Time - the maximum propagation time, after which the segment will end regardless of whether the stopping conditions have been satisfied. Uses Time Dimension.
`enable_max_propagation_time`	Enable Maximum Propagation Time - apply the maximum propagation time.
`enable_warning_message`	Issue a warning message if propagation is stopped by the Maximum Propagation Time parameter.
`enable_center_burn`	Get or set the option to start the maneuver half the time before the previous segment ended. This property is only available for use with a duration stopping condition.
`bias`	Get or set the value by which to adjust the centering of the burn. A positive value will center the burn after the previous segment ends by the amount specified in the Burn Center Bias field. Uses Time Dimension.
`override_max_propagation_time`	Override Maximum Propagation Time - if there is a duration or epoch stopping condition that occurs after the maximum propagation time, ignore the maximum propagation time.
`should_stop_for_initially_surpassed_epoch_stopping_conditions`	Stop immediately if propagation begins beyond an active epoch stopping condition.
`should_reinitialize_stm_at_start_of_segment_propagation`	If this segment is propagating the state transition matrix, reset it to the identity matrix at the start of the segment.

Import detail#

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

Property detail#

property ManeuverFinitePropagator.propagator_name: str#: Get or set the propagator.

property ManeuverFinitePropagator.stopping_conditions: StoppingConditionCollection#: Get the stopping conditions list.

property ManeuverFinitePropagator.min_propagation_time: float#: Minimum Propagation Time - the minimum time that must elapse from the beginning of the segment until Astrogator will begin checking stopping conditions for satisfaction. Uses Time Dimension.

property ManeuverFinitePropagator.max_propagation_time: float#: Maximum Propagation Time - the maximum propagation time, after which the segment will end regardless of whether the stopping conditions have been satisfied. Uses Time Dimension.

property ManeuverFinitePropagator.enable_max_propagation_time: bool#: Enable Maximum Propagation Time - apply the maximum propagation time.

property ManeuverFinitePropagator.enable_warning_message: bool#: Issue a warning message if propagation is stopped by the Maximum Propagation Time parameter.

property ManeuverFinitePropagator.enable_center_burn: bool#: Get or set the option to start the maneuver half the time before the previous segment ended. This property is only available for use with a duration stopping condition.

property ManeuverFinitePropagator.bias: float#: Get or set the value by which to adjust the centering of the burn. A positive value will center the burn after the previous segment ends by the amount specified in the Burn Center Bias field. Uses Time Dimension.

property ManeuverFinitePropagator.override_max_propagation_time: bool#: Override Maximum Propagation Time - if there is a duration or epoch stopping condition that occurs after the maximum propagation time, ignore the maximum propagation time.

property ManeuverFinitePropagator.should_stop_for_initially_surpassed_epoch_stopping_conditions: bool#: Stop immediately if propagation begins beyond an active epoch stopping condition.

property ManeuverFinitePropagator.should_reinitialize_stm_at_start_of_segment_propagation: bool#: If this segment is propagating the state transition matrix, reset it to the identity matrix at the start of the segment.