A new guidance strategy in aerodynamic ascent path using air-breathing propulsion

Takayuki Yamamoto, Jun'ichiro Kawaguchi

研究成果: Conference contribution

1 被引用数 (Scopus)

抄録

The paper proposes the new guidance strategy in the aerodynamic ascent path. This guidance form has only four parameters comprised of Linear and Logarithmic functions. And the paper presents the guidance results for the practical application cases with certain constraints. The results show the guidance is well performed and satisfies the terminal boundary conditions specified. This guidance strategy does not include the optimization process aboard but solves a simple two-by-two linear algebraic equations along with forward integration. This strategy does guarantee the robust and real-time solutions, excluding any optimization process, and it is concluded quite practical.

本文言語English
ホスト出版物のタイトルAstrodynamics 2005 - Advances in the Astronautical Sciences - Proceedings of the AAS/AIAA Astrodynamics Conference
ページ1565-1576
ページ数12
出版ステータスPublished - 2006
外部発表はい
イベントAstrodynamics 2005 - Advances in the Astronautical Sciences - Proceedings of the AAS/AIAA Astrodynamics Conference - South Lake Tahoe, CA, United States
継続期間: 2005 8 72005 8 11

出版物シリーズ

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

Conference

ConferenceAstrodynamics 2005 - Advances in the Astronautical Sciences - Proceedings of the AAS/AIAA Astrodynamics Conference
国/地域United States
CitySouth Lake Tahoe, CA
Period05/8/705/8/11

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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