Nonlinear attractive sets under optimal feedback control in the hill three-body problem

Mai Bando, Daniel J. Scheeres

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

抄録

Trajectory design combining low-thrust and the three-body problem is a challenging area for study. This paper investigates the combination of optimal feedback control with the dynamical structure of the three-body problem. For the nonlinear system, the attractive set of an equilibrium point or a periodic orbit under optimal control is described by the Hamilton-Jacobi-Bellman partial differential equation. We obtain the solution to the Hamilton-Jacobi-Bellman equation by solving the truncation problem successively.

本文言語英語
ホスト出版物のタイトルAIAA/AAS Astrodynamics Specialist Conference, 2016
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624104459
DOI
出版ステータス出版済み - 2016
イベントAIAA/AAS Astrodynamics Specialist Conference, 2016 - Long Beach, 米国
継続期間: 9 13 20169 16 2016

出版物シリーズ

名前AIAA/AAS Astrodynamics Specialist Conference, 2016

その他

その他AIAA/AAS Astrodynamics Specialist Conference, 2016
Country米国
CityLong Beach
Period9/13/169/16/16

All Science Journal Classification (ASJC) codes

  • Astronomy and Astrophysics
  • Aerospace Engineering

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