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Librational Damping of A Gravity Orientated System using Solar Radiation Pressure

Published online by Cambridge University Press:  04 July 2016

V. J. Modi
Affiliation:
The University of British Columbia, Vancouver, Canada
R. C. Flanagan
Affiliation:
The University of British Columbia, Vancouver, Canada

Extract

For many space applications, 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 librational 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
Copyright
Copyright © Royal Aeronautical Society 1971 

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References

1. Klemperer, W. B. and Baker, R. M. Jr. Satellite Librations. Astronaut, Acta., Vol 3, No 1, pp. 1627, January 1957.Google Scholar
2. Schechter, Hans B. Dumbbell Librations in Elliptic Orbits AIAA J, Vol 2, No 6, pp. 10001003, 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, pp. 179192. Proceedings of the XVIIth International Astronautical Congress, Vol IV, 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, pp. 109120. Proceedings of the XVIIIth International Astronautical Congress, Pergamon Press, London, 1968.Google Scholar
5. Flanagan, R. C. and Modi, V. J. Radiation Forces on a Flat Plate in Close Earth Orbits, pp. 249250. Proceedings of the Second Canadian Congress of Applied Mechanics, Waterloo, Canada, 1969.Google Scholar
6. Roberson, R. E. Attitude Control of a Satellite Vehicle— An Outline of the Problem, pp.317339. Proceedings of the Vlllth International Astronautical Congress, 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. Clancy, T. F. and Mitchell, T. P. Effects of Radiation Forces on the Attitude of an Artificial Earth Satellite, AIAA J., Vol 2, No 3, pp. 517524, 1964.Google Scholar
9. Flanagan, R. C and Modi, V. J. Radiation Forces on a Flat Plate in Close Earth Orbits, pp. 249250. Proceedings of the Canadian Congress of Applied Mechanics, Editor: Lind, N. C., University of Waterloo, Waterloo, Ontario, 1969.Google Scholar
10. Modi, V. J. and Flanagan, R. C. Librational Stability of a Gravity Orientated System in the Presence of Radiation Pressure, In Press, Journal of Applied Mechanics, American Society of Mechanical Engineers.Google Scholar
11. Flanagan, R. C. and Modi, V. J. Attitude Dynamics of a Gravity Orientated Satellite under the Influence of Solar Radiation Pressure, Aeronautical Journal, Royal Aeronautical Society, Vol 74, No 718, pp. 835841, October 1970.Google Scholar
12. Garwin, L. I. Solar Sailing—A Practical Method of Propulsion within the Solar System, Jet Propulsion, Vol 28, pp. 188190, 1958.Google Scholar
13. Sohn, R. L. Attitude Stabilization by Means of Solar Radiation Pressure, ARS Journal, Vol 29, No 5, pp. 371373, 1959.Google Scholar
14. Newton, R. R. Stabilizing a Spherical Satellite by Radiation Pressure, ARS Journal, Vol 30, No 12, pp. 11751177, 1960.Google Scholar
15. Villers, P. and Olha, W. A Solar Sail Attitude Stabilizer for Satellites and Interplanetary Probes, ARS Paper 2251-61, 1961.Google Scholar
16. Windeknecht, T. G. A Simple System for Sun Orientation of a Spinning Satellite, IAS Paper 61-204-1898, 1961.Google Scholar
17. Mallach, E. G. Solar Pressure Damping of the Librations of a Gravity Gradient Orientated Satellite, AIAA Student Journal, Vol 4, No 4, pp. 143147. December 1966.Google Scholar
18. Paul, B. Planar Librations of an Extensible Dumbbell Satellite, AIAA Journal, Vol 1, No 2, pp. 411418. February 1963.Google Scholar
19. Modi, V. J. and Brereton, R. C. The Planar Motion of a Damped Satellite, CASI Trans., Vol 2, No 1, pp. 4448, March 1969.Google Scholar