Attitude Error of Satellite Due to Gravity Gradient Boom-Reference-Cited by-同舟云学术

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Attitude Error of Satellite Due to Gravity Gradient Boom

Published:2003 Issue:599 Volume:51 Page:659-666
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Ueno Seiya

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/51/599/51_599_659/_pdf

Reference20 articles.

1. Stabilization system analysis and performance of the Geos-A gravity-gradient satellite

2. Attitude performance of the GEOS-II gravity- gradient spacecraft

3. Satellite attitude control using a torqued, 2-axis-gimbaled boom as the actuator.

4. Possible effects of boom flutter on the attitude dynamics of the OV1-10 satellite.

5. 5) 茂原正道:宇宙システム概論—衛星の設計と開発,培風館,東京,1995, p. 203.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Parametric excitation induced by solar pressure torque on the roll-yaw attitude motion of a gravity-gradient stabilized spacecraft;Celestial Mechanics and Dynamical Astronomy;2010-10-24

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