Stability of plane librations of near-earth satellite subjected to aerodynamic and gravity gradient torques is examined for general case of eccentric orbit; stability boundaries are determined numerically and presented in terms of nondimensional configuration and orbit parameters; examples of both stable and unstable angular motions; configurations are analyzed to illustrate degree of aerodynamic attitude stabilization possible in orbit with practical vehicles.
Dynamic stability of aerodynamically responsive satellites
J Aerospace Sciences
Journal of the Aero/Space Sciences ; 29 , n 10
1962
Article (Journal)
English
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