Low-thrust trajectory optimization using second-order generating functions

Mai Bando, Hiroshi Yamakawa

研究成果: 著書/レポートタイプへの貢献会議での発言

1 引用 (Scopus)

抜粋

The optimal control problem of a spacecraft using continuous thrust where the terminal state and time interval are explicitly given is considered. We consider a new robust controller to the spacecraft rendezvous problem. Optimal rendezvous problem using continuous low-thrust is treated as optimal control problem and H control. Using the property that both problems can be treated as two-point boundary value problem (TPVBP) of Hamiltonian system, we formulate the linear quadratic control with worst case disturbance rejection and worst case initial condition related by generating functions. Numerical simulations are given to illustrate the theory.

元の言語英語
ホスト出版物のタイトルProceedings of SICE Annual Conference 2010, SICE 2010 - Final Program and Papers
出版者Society of Instrument and Control Engineers (SICE)
ページ804-810
ページ数7
ISBN(印刷物)9784907764364
出版物ステータス出版済み - 1 1 2010
外部発表Yes

出版物シリーズ

名前Proceedings of the SICE Annual Conference

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Computer Science Applications
  • Electrical and Electronic Engineering

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  • これを引用

    Bando, M., & Yamakawa, H. (2010). Low-thrust trajectory optimization using second-order generating functions. : Proceedings of SICE Annual Conference 2010, SICE 2010 - Final Program and Papers (pp. 804-810). [5603000] (Proceedings of the SICE Annual Conference). Society of Instrument and Control Engineers (SICE).