Application of global solution of Hamilton-Jacobi equations to optimal low-thrust multiple rendezvous problem

Mai Bando, Hiroshi Yamakawa

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

This paper presents a procedure to design multiple rendezvous missions. We propose a new low-thrust trajectory optimization method to find the optimal trajectory in analytical form. The resulting control law is a feedback control, so that it is effective in overcoming sensitivities to small variations in initial orbit and thrust profile. This study determines the optimal approach to find an effective control law to sequential transfer problem. For comparison, optimal sequence using impulsive and continuous thrust method are investigated. Our approaches are illustrated through the trajectory design of the multiple flyby mission and resulting fuel costs are compared.

本文言語英語
ホスト出版物のタイトル61st International Astronautical Congress 2010, IAC 2010
ページ9611-9618
ページ数8
出版ステータス出版済み - 12 1 2010
外部発表はい
イベント61st International Astronautical Congress 2010, IAC 2010 - Prague, チェコ共和国
継続期間: 9 27 201010 1 2010

出版物シリーズ

名前61st International Astronautical Congress 2010, IAC 2010
12

その他

その他61st International Astronautical Congress 2010, IAC 2010
Countryチェコ共和国
CityPrague
Period9/27/1010/1/10

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics

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