ManeuverOptimalFiniteFinalBoundaryConditions#

class ansys.stk.core.stkobjects.astrogator.ManeuverOptimalFiniteFinalBoundaryConditions#: Properties of final boundary conditions for optimal finite maneuver.

Overview#

Properties

`set_from_final_guess`	Set initial boundary conditions from initial guess.
`a`	Bound limits for element a.
`h`	Bound limits for element h.
`k`	Bound limits for element k.
`p`	Bound limits for element p.
`q`	Bound limits for element q.
`l`	Bound limits for element L.
`lower_delta_final_time`	Lower delta for final time.
`upper_delta_final_time`	Upper delta for final time.
`provide_runtime_type_info`	Return the RuntimeTypeInfo interface to access properties at runtime.

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

property ManeuverOptimalFiniteFinalBoundaryConditions.set_from_final_guess: bool#: Set initial boundary conditions from initial guess.

property ManeuverOptimalFiniteFinalBoundaryConditions.a: ManeuverOptimalFiniteBounds#: Bound limits for element a.

property ManeuverOptimalFiniteFinalBoundaryConditions.h: ManeuverOptimalFiniteBounds#: Bound limits for element h.

property ManeuverOptimalFiniteFinalBoundaryConditions.k: ManeuverOptimalFiniteBounds#: Bound limits for element k.

property ManeuverOptimalFiniteFinalBoundaryConditions.p: ManeuverOptimalFiniteBounds#: Bound limits for element p.

property ManeuverOptimalFiniteFinalBoundaryConditions.q: ManeuverOptimalFiniteBounds#: Bound limits for element q.

property ManeuverOptimalFiniteFinalBoundaryConditions.l: ManeuverOptimalFiniteBounds#: Bound limits for element L.

property ManeuverOptimalFiniteFinalBoundaryConditions.lower_delta_final_time: float#: Lower delta for final time.

property ManeuverOptimalFiniteFinalBoundaryConditions.upper_delta_final_time: float#: Upper delta for final time.

property ManeuverOptimalFiniteFinalBoundaryConditions.provide_runtime_type_info: RuntimeTypeInfo#: Return the RuntimeTypeInfo interface to access properties at runtime.