Guidance and navigation of hayabusa spacecraft for asteroid exploration and sample return mission

Takashi Kubota, Tatsuaki Hashimoto, Ju N.Ichiro Kawaguchi, Masashi Uo, Ke N.Ichi Shirakawa

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

26 Citations (Scopus)

Abstract

The Japanese asteroid exploration spacecraft Hayabusa autonomously performed touchdown two times in November 2005. The autonomous guidance and navigation capability is installed aboard the spacecraft. The GNC system collects the laser altimeter, laser range finders and navigation cameras information aboard and is designed to estimate where the spacecraft is and to decide the path correction maneuvers. The programmed function includes the image processing designed to detect an artificial target marker location to approach and cancel the relative velocity. A terrain alignment maneuver is also accomplished by both altitude and attitude control. This paper presents how autonomous guidance and navigation was performed in Hayabusa mission.

Original languageEnglish
Title of host publication2006 SICE-ICASE International Joint Conference
Pages2793-2796
Number of pages4
DOIs
Publication statusPublished - 2006
Externally publishedYes
Event2006 SICE-ICASE International Joint Conference - Busan, Korea, Republic of
Duration: 2006 Oct 182006 Oct 21

Publication series

Name2006 SICE-ICASE International Joint Conference

Other

Other2006 SICE-ICASE International Joint Conference
Country/TerritoryKorea, Republic of
CityBusan
Period06/10/1806/10/21

Keywords

  • Asteroid exploration
  • Autonomous descent
  • GNC
  • Hayabusa
  • Touchdown

ASJC Scopus subject areas

  • Computer Science Applications
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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