Vibration Isolation Platform for Control Moment Gyroscopes on Satellites
Author:
Affiliation:
1. Ph.D. Student, Dept. of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing, China 100191 (corresponding author).
2. Professor, Dept. of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing, China 100191.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000156
Reference32 articles.
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3. Basdogan I. Grogan R. Kissil A. Sigrist N. and Sievers L. (2000). “Preliminary optical performance analysis of the space interferometer mission using an integrated modeling methodology.” Proc. Control of Vibration and Noise-New Millennium: Int. Mechanical Engineering Congress & 6th Exposition Biennial Symp. on Active Control of Vibration and Noise Orlando FL.
4. Baudoin A. Boussarie E. Damilano P. Rim G. and Caltagirone F. (2001). “Pléiades: A multi mission and multi cooperative program.” Proc. 52nd Int. Astronautical Congress . IAF Toulouse France.
5. Vibration Isolator for Large Space Telescopes
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