Stability of Satellite Attitude in a Central Force Field
The subsequent stability analyses are for absolutely rigid satellites of finite size in the gravitational field of a point master. The term gravity gradient stabilization (or GG stabilization) is used frequently by space engineers for satellites stabilized by taking advantage of the gradient of the gravitational field surrounding the master, the gradient of the field being none other than the Kepler force K, which, because of the finite size of the satellite, also exerts a torque on the satellite.
KeywordsCircular Orbit Satellite Attitude Absolute Angular Velocity Angular Velocity Component Cardan Angle
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- 1.Hughes, P.C. Spacecraft Attitude Dynamics, Wiley & Sons, 1985, 576 pp.Google Scholar
- 2.Kane, T.R.; E.L. Marsh; W.G. Wilson. “Letters to the Editor,” Journal of the Astronautical Sciences, 108–109.Google Scholar
- 4.Thomson, W.T. “Spin Stabilization of Attitude against Gravity Torque,” Journal of the Astronautical Sciences, 9, 1, 1962, 31–33.Google Scholar
- 5.Tyc, G. “A Method of Stability Analysis for Systems of Linear Differential Equations with Periodic Coefficients,” M.A.S.c. Thesis, University of Toronto, 1987, 164 pp.Google Scholar
- 7.Zlatoustov, V.A.; D.E. Okhotsimsky; V.A. Sarychev; A.P. Torzhevsky. “Investigation of Satellite Oscillations in the Plane of an Elliptic Orbit,” Proceedings (Ed. H. Görtier), 11th International Congress of Applied Mechanics, Munich, 1964, Springer-Verlag, 1966, 436–439.Google Scholar