Co-state initialization for the minimum-time low-thrust trajectory optimization-Reference-Cited by-同舟云学术

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Co-state initialization for the minimum-time low-thrust trajectory optimization

Published:2017-05 Issue:9 Volume:59 Page:2360-2373
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Taheri Ehsan,Li Nan I.,Kolmanovsky Ilya

Funder

National Science Foundation

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference33 articles.

1. Dynamic-size multiple populations genetic algorithm for multigravity-assist trajectory optimization;Abdelkhalik;J. Guid. Control Dynam.,2012

2. New smoothing techniques for solving bang–bang optimal control problems – numerical results and statistical interpretation;Bertrand;Opt. Control Appl. Methods,2002

3. Survey of numerical methods for trajectory optimization;Betts;J. Guid. Control Dynam.,1998

4. Automated design of multiphase space missions using hybrid optimal control;Chilan;J. Guid. Control Dynam.,2013

5. Adjoint-control transformations for solving practical optimal control problems;Dixon;Opt. Control Appl. Methods,1981

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