DYNAMICS, CONTROL AND STRUCTURAL FLEXIBILITY RESULTS FROM THE HERMES MISSION-Reference-Cited by-同舟云学术

DYNAMICS, CONTROL AND STRUCTURAL FLEXIBILITY RESULTS FROM THE HERMES MISSION

Published:1979 Issue: Volume: Page:397-411
ISSN:
Container-title:Astronautics for Peace and Human Progress
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Author:

Vigneron F.R.

Publisher

Elsevier

Reference13 articles.

1. Bassett, D.A. (1976). Ground Controlled Conversion of the Communications Technology Satellite (CTS) from Spinning Mode to Three-Axis Stabilized Mode. AIAA Paper No. 76–1928.

2. Davies, N.G. (1977). The HERMES Mission. Royal Society of Canada 20th Symposium ‘Symposium on HERMES - Its Performance and Applications”. Ottawa, Canada. IBSN 0–920064-12–4. Vol. 1, pp. 11–42.

3. Franklin, C.A. and E.H. Davidson (1973). A High Power Communications Technology Satellite for the 12 and 14 GHz Bands. AIAA Progress in Aeronautics and Astronautics.

4. Garg, S.C. and Others (1978). Flight Results on Structural Dynamics from Hermes. Submitted to AIAA for publication in 1978.

5. Gore, J.V. and K.P. Bogus (1977). The Flight Performance of the Hermes Power Subsystem and Flexible Solar Arrays. Royal Society of Canada 20th Symposium. Symposium on Hermes - Its Peformance and Applications. Ottawa, Canada. IBSN 0–920064-12–4. pp. 33–50.

Cited by 3 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. Damping synthesis for a spacecraft using substructure and component data;Journal of Spacecraft and Rockets;1986-03

2. MODAL DAMPING MEASUREMENT OF MOS-1 SOLAR ARRAY PADDLE;Automatic Control in Space 1985;1986

3. Hermes satellite /CTS/ - Performance and operations summary;8th Communications Satellite Systems Conference;1980-04-20