Libration Control of a Tethered System in Elliptic Orbits.-Reference-Cited by-同舟云学术

Libration Control of a Tethered System in Elliptic Orbits.

Published:2001 Issue:567 Volume:49 Page:130-134
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:

TAKEICHI Noboru,NATORI M.C.,OKUIZUMI Nobukatsu

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/49/567/49_567_130/_pdf

Reference15 articles.

1. 2) Oyama, K.I., Sasaki, S., Su, Y. and Balan, N.: Feasibility Study on a Tethered Satellite System, Proc. 2nd Int. Workshop Application of Tethered Systems in Space, ISAS, 1994.

2. Periodic solutions associated with the gravity- gradient-oriented system. I - Analytical and numerical determination.

3. Periodic solutions associated with the gravity- gradient-oriented system. II - Stability analysis.

4. 5) Karasopoulos, H.A. and Richardson, D.L.: Chaos in the Pitch Equation of Motion for the Gravity-Gradient Satellite, AIAA-92-4369, AIAA/AAS Astrodynamics Conference, Hilton Head, 1992.

5. 6) Karasopoulos, H.A. and Richardson, D.L.: Numerical Investigation of Chaos in the Attitude Motion of a Gravity-Gradient Satellite, AAS 93-581, AIAA/AAS Astrodynamics Conference, Victoria, Canada, 1993.

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