A new optimal orbit control for two-point boundary-value problem using generating functions

Mai Bando, Hiroshi Yamakawa

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

12 被引用数 (Scopus)

抄録

The optimal control problem of a spacecraft using impulsive and continuous thrust where the terminal state and time interval are explicitly given is considered. Using a recently developed technique based on Hamilton-Jacobi theory, we develop a method to approximate the solution of the Hamilton-Jacobi equation which can solve the two-point boundary-value problem. The proposed method is based on the successive approximation and Galerkin spectral method with Chebyshev polynomials. This approach is expected to derive the analytical solution of the optimal control problem in the large domain. Numerical simulation is given to illustrate the theory.

本文言語英語
ホスト出版物のタイトルSpaceflight Mechanics 2009 - Advances in the Astronautical Sciences
ホスト出版物のサブタイトルProceedings of the 19th AAS/AIAA Space Flight Mechanics Meeting
ページ245-260
ページ数16
出版ステータス出版済み - 12 1 2009
外部発表はい
イベント19th AAS/AIAA Space Flight Mechanics Meeting - Savannah, GA, 米国
継続期間: 2 8 20092 12 2009

出版物シリーズ

名前Advances in the Astronautical Sciences
134
ISSN(印刷版)0065-3438

その他

その他19th AAS/AIAA Space Flight Mechanics Meeting
国/地域米国
CitySavannah, GA
Period2/8/092/12/09

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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