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On concomitant satellite orbital maintenance

科研成果: 期刊稿件文章同行评审

6 引用 (Scopus)

摘要

Two-impulse control is used for concomitant orbital control. Based on concomitant motion sate transferring equation, analytic solution of two-impulse concomitant orbital transfer is derived, the control variables are optimized by means of genetic algorithm, and optimal transfer time and trajectories are gained.

源语言英语
页(从-至)398-400
页数3
期刊Yuhang Xuebao/Journal of Astronautics
25
4
出版状态已出版 - 7月 2004

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