Gravitational orbit-attitude coupling for very large spacecraft
Author:
Affiliation:
1. Toronto, University, Toronto, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-1402
Reference11 articles.
1. .&!eirovitch, L. "Cm the Effect or'Higher-Order faartia Integrals on the Attitude Stability of Earth-pointing SatellitesJf1Journal of Astronautical Sciences, Vol.XV, Er'o.1,Jan.Feb. 1968, pp.14-18.
2. Sincarsin, G. B. "Gravitational Orbit-Attitucie Coupling and Penumbral Solar-GradientTarques for Very Large Spacecraft," UTL.6 Report 265, 1982.
3. Hughes, P. C. "Attitude Dynamics of Spacecraft** (to be published), 1982.
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