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KIAM Preprint  98, Moscow, 2018
Authors: Tselousova A.A., Shirobokov M.G., Trofimov S.P.
Comparison of two direct interplanetary trajectory optimization techniques
In this work, two direct methods of low-thrust trajectory optimization are implemented and compared. The first method is based on optimization of the thrust acceleration, whereas the second method optimizes the impulses that approximate the thrust arcs. The methods are applied to the sample problem of a transfer from the Earth to Mars. The results are obtained on a personal computer in MATLAB and on a multiprocessing computing system.
trajectory design, low thrust, direct optimization method, shooting method, optimal control, cluster K-60
Publication language: russian,  pages: 24
Research direction:
Theoretical and applied problems of mechanics
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About authors:
  • Tselousova Anastasiia Alexandrovna, 
  • Shirobokov Maksim Gennadievich, RAS
  • Trofimov Sergey Pavlovich, RAS