Satellite position and attitude control by on-off thrusters considering mass change

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

抄録

This paper deals with the two-dimensional position and attitude control of a satellite by on-off thrusters which are fixed to the satellite's body. Since the thrusters generate constant and unilateral forces, the equations of motion form nonholonomic constraint and cannot be integrated. Furthermore, the satellite's mass changes due to the fuel consumption. Utilizing Fresnel integrals and the partial integrals, we derive the approximate analytic solution considering the satellite's mass change to achieve a specified satellite's position and attitude. The accuracy of the proposed approximate technique is verified by applying it to a condition considered in SLIM project of JAXA.

本文言語英語
ホスト出版物のタイトルASTRODYNAMICS 2011 - Advances in the Astronautical Sciences
ホスト出版物のサブタイトルProceedings of the AAS/AIAA Astrodynamics Specialist Conference
ページ2953-2964
ページ数12
142
出版ステータス出版済み - 2012
イベント2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011 - Girdwood, AK, 米国
継続期間: 7 31 20118 4 2011

その他

その他2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011
国/地域米国
CityGirdwood, AK
Period7/31/118/4/11

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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