Attitude control challenges and solutions for Hayabusa spacecraft

Masashi Uo, Kenichi Shirakawa, Tatsuaki Hashimoto, Takashi Kubota, Jun'ichiro Kawaguchi

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

Abstract

Hayabusa attempted to touch-down two times in November, 2005 after two years of cruising and two months of proximity observation around ITOKAWA. One of three reaction wheels failed in late July of 2005, and the second wheel failed in early October. While the attitude stabilization logic with two wheels was inherent in the onboard system, the stabilization with one wheel required the use of onboard re-programming function and special ground support operations. This paper describes how the attitude control system and operation were adapted to cope with the loss of reaction wheels, along with the introduction of attitude control system that was designed to realize various attitude functions with minimum onboard resources.

Original languageEnglish
Title of host publicationCollection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006
Pages1342-1351
Number of pages10
Publication statusPublished - 2006
Externally publishedYes
EventAIAA/AAS Astrodynamics Specialist Conference, 2006 - Keystone, CO, United States
Duration: 2006 Aug 212006 Aug 24

Publication series

NameCollection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006
Volume2

Conference

ConferenceAIAA/AAS Astrodynamics Specialist Conference, 2006
CountryUnited States
CityKeystone, CO
Period06/8/2106/8/24

ASJC Scopus subject areas

  • Engineering(all)

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