New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation

From MaRDI portal
Publication:5695548

DOI10.1002/oca.709zbMath1072.49502OpenAlexW2021762091MaRDI QIDQ5695548

No author found.

Publication date: 13 October 2005

Published in: Optimal Control Applications and Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/oca.709



Lua error in Module:PublicationMSCList at line 37: attempt to index local 'msc_result' (a nil value).


Related Items (24)

A robust pseudospectral method for numerical solution of nonlinear optimal control problemsCombined homotopy and neighboring extremal optimal controlDifferential continuation for regular optimal control problemsMinimum fuel control of the planar circular restricted three-body problemFuel optimization for low-thrust Earth-Moon transfer via indirect optimal controlA survey on orbital dynamics and navigation of asteroid missionsAdjoints estimation methods for impulsive Moon-to-Earth trajectories in the restricted three-body problemA symplectic sequence iteration approach for nonlinear optimal control problems with state-control constraintsA COMBINED ADAPTIVE CONTROL PARAMETRIZATION AND HOMOTOPY CONTINUATION TECHNIQUE FOR THE NUMERICAL SOLUTION OF BANG–BANG OPTIMAL CONTROL PROBLEMSState-Dependent Temperature Control for Langevin DiffusionsEpsilon-Trig regularization method for bang-bang optimal control problemsA continuous implementation of a second-variation optimal control method for space trajectory problemsSolution space exploration of low-thrust minimum-time trajectory optimization by combining two homotopiesAnalysis of the inertially symmetric rigid spacecraft time-optimal three-axis reorientationInterplanetary gravity-assist fuel-optimal trajectory optimization with planetary and Solar radiation pressure perturbationsA variation evolving method for optimal control computationTime-optimal reorientation of the rigid spacecraft using a pseudospectral method integrated homotopic approachLow-thrust transfers to southern \(L_2\) near-rectilinear halo orbits facilitated by invariant manifoldsA two-phase computational scheme for solving bang-bang control problemsBang-bang optimal control for differentially flat systems using mapped pseudospectral method and analytic homotopic approachUsing Homotopy Method to Solve Bang–Bang Optimal Control ProblemsA modified pseudospectral scheme for accurate solution of Bang-Bang optimal control problemsTentative Solutions for Indirect Optimization of Spacecraft TrajectoriesFlatness-Based Low-Thrust Trajectory Optimization for Spacecraft Proximity Operations



Cites Work


This page was built for publication: New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation