ManeuverOptimalFiniteInitialBoundaryConditions#

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

Properties of initial boundary conditions for optimal finite maneuver.

Overview#

set_from_initial_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.

provide_runtime_type_info

Return the RuntimeTypeInfo interface to access properties at runtime.

Import detail#

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

Property detail#

property ManeuverOptimalFiniteInitialBoundaryConditions.set_from_initial_guess: bool#

Set initial boundary conditions from initial guess.

property ManeuverOptimalFiniteInitialBoundaryConditions.a: ManeuverOptimalFiniteBounds#

Bound limits for element a.

property ManeuverOptimalFiniteInitialBoundaryConditions.h: ManeuverOptimalFiniteBounds#

Bound limits for element h.

property ManeuverOptimalFiniteInitialBoundaryConditions.k: ManeuverOptimalFiniteBounds#

Bound limits for element k.

property ManeuverOptimalFiniteInitialBoundaryConditions.p: ManeuverOptimalFiniteBounds#

Bound limits for element p.

property ManeuverOptimalFiniteInitialBoundaryConditions.q: ManeuverOptimalFiniteBounds#

Bound limits for element q.

property ManeuverOptimalFiniteInitialBoundaryConditions.l: ManeuverOptimalFiniteBounds#

Bound limits for element L.

property ManeuverOptimalFiniteInitialBoundaryConditions.provide_runtime_type_info: RuntimeTypeInfo#

Return the RuntimeTypeInfo interface to access properties at runtime.