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Optimal impulsive thrust trajectories for satellite formation via improved brainstorm optimization

  • Olukunle Kolawole Soyinka*
  • , Haibin Duan
  • *此作品的通讯作者
  • Beihang University
  • National Space Research and Development Agency

科研成果: 书/报告/会议事项章节章节同行评审

摘要

The optimization of the satellite trajectory is a product of the control thrust optimization. Using the Lambert theory formulation this paper considers the problem of a minimum fuel solution of the Lambert formulation by making use of Brainstorm Optimization (BSO). The traditional use of the Lambert formulation for generating control inputs typically pursues time dependent solutions. This paper adapted this formulation to satellite formation control to achieve fuel minimization. The numerical simulations show the feasibility of our method in obtaining minimum fuel solutions of the lambert formulation in contrast to the usual minimum time solution.

源语言英语
主期刊名Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
出版商Springer Verlag
491-499
页数9
DOI
出版状态已出版 - 2016

出版系列

姓名Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
9712 LNCS
ISSN(印刷版)0302-9743
ISSN(电子版)1611-3349

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