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

Takayuki Yamamoto, Jun'ichiro Kawaguchi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

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.

Original languageEnglish
Title of host publicationAstrodynamics 2005 - Advances in the Astronautical Sciences - Proceedings of the AAS/AIAA Astrodynamics Conference
Pages1565-1576
Number of pages12
Publication statusPublished - 2006
Externally publishedYes
EventAstrodynamics 2005 - Advances in the Astronautical Sciences - Proceedings of the AAS/AIAA Astrodynamics Conference - South Lake Tahoe, CA, United States
Duration: 2005 Aug 72005 Aug 11

Publication series

NameAdvances in the Astronautical Sciences
Volume123 II
ISSN (Print)0065-3438

Conference

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

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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