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Attitude Dynamics of a Gravity Orientated Satellite under the Influence of Solar Radiation Pressure

Published online by Cambridge University Press:  04 July 2016

R. C. Flanagan  and
V. J. Modi
R. C. Flanagan
Affiliation:
Dept of Mechanical Engineering, The University of British Columbia, Vancouver
V. J. Modi
Affiliation:
Dept of Mechanical Engineering, The University of British Columbia, Vancouver
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Extract

For many space applications, such as communication, weather, military, and scientific experiment satellites scanning precise regions, it is necessary to maintain a satellite in a fixed orientation relative to the earth. Unfortunately, a correctly positioned satellite deviates with time from this preferred orientation due to perturbing environmental forces. This explains considerable interest in libra-tional stability study in recent times.

Among the numerous methods developed for librational control, a passive technique depending on the gradient of the gravitational field has gained attention. Depending on the orbital distance, environmental effects, such as, aerodynamic, radiation, and magnetic torques, become significant compared to the gravity-gradient restoring moment. A need to determine the influence of these disturbing forces is thus evident.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 74 , Issue 718 , October 1970 , pp. 835 - 841
Copyright
Copyright © Royal Aeronautical Society 1970 

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References

1. Klemperer, W. B. and Baker, R. M. Jr. Satellite Libration, Astronaut. Acta, Vol 3, No 1, pp 16–27. January 1957.Google Scholar
2. Schechter, H. B. Dumbbell Librations in Elliptic Orbits. AIAA Journal, Vol 2, No 6, pp 1000–1003. June 1964.Google Scholar
3. Brereton, R. C. and Modi, V. J. Stability of the Planar Librational Motion of a Satellite in an Elliptic Orbit. Proceedings of the XVIIlth International Astronautical Congress, Vol IV, pp 179–192. Gordon and Breach Science Publishers, Inc, New York, 1967.Google Scholar
4. Modi, V. J. and Brereton, R. C. Stability of a Dumbbell Satellite in a Circular Orbit During Coupled Librational Motions. Proceedings of the XVIIlth International Astro-nautical Congress, pp.109–120. Pergamon Press, London, 1968.Google Scholar
5. Flanagan, R. C. and Modi, V. J. Radiation Forces on a Flat Plate in Close Earth Orbits. Proceedings of the Second Canadian Congress of Applied Mechanics, pp 249– 250. Waterloo, Canada, 1969.Google Scholar
6. Roberson, R. E. Attitude Control of a Satellite Vehicle— an Outline of the Problem. Proceedings of the Vlllth International Astronautical Congress, pp 317–339. Wein- Springer-Verlag, Berlin, 1958.Google Scholar
7. Hall, H. B. The Effects of Radiation Force on Satellites of Convex Shape.NASA TN D-604, 1961.Google Scholar
8. Cunningham, F. G. Power Input to a Small Flat Plate from a Diffusely Radiating Sphere, with Application to Earth Satellites.NASA TN D-710, 1961.Google Scholar
9. Cunningham, F. G. EarthReflectedSolar Radiation Input to Spherical Satellites.NASA TN D-1099, 1961.Google Scholar
10. Clancy, J. F. and Mitchell, T. P. Effects of Radiation Forces on the Attitude of an Artificial Earth Satellite. AIAA Journal, Vol 2, No 3, pp 517–524, 1964.Google Scholar
11. Flanagan, R. C. and Modi, V. J. Radiation Forces on a Flat Plate in Eliptic Near Earth Orbit. CASI Transactions, in press.Google Scholar
12. Modi, V. J. and Flanagan, R. C. Effect of Environmental Forces on the Attitude Dynamics of Gravity Oriented Satellites. Presented for publication in The Aeronautical Journal of the Royal Aeronautical Society.Google Scholar
13. Moran, J. P. Effects of Plane Librations on the Orbital Motion of a Dumbbell Satellite. ARS Journal, Vol 31, No 8, pp 1089–1096.August 1961.Google Scholar
14. Yu, E. Y. Long-TermCouplingEffectsBetweenthe Librational and Orbital Motions of a Satellite. AIAA Journal, Vol 2, No 3, pp 553-55. March 1964.Google Scholar
15. Hénon, M. and Heiles, C. The Applicability of Third Integral of Motion: Some Numerical Experiments. Astronomical Journal, Vol 69, No 1, pp 73–79. February 1964.Google Scholar
16. Moser, Jurgen. Perturbation Theory for Almost Periodic Solutions for Undamped Nonlinear Differential Equations. International Symposium on Nonlinear Differential Equations and Nonlinear Mechanics, pp 71–79. Edited by LaSalle, J. P. and Lefschetz, S.. Academic Press, New York, 1963.Google Scholar