The stability criteria for a missile on a pendulous support are derived for the case of parametrically excited motions of the support. The suspension system is described by two linear second-order differential equations with a periodic coefficient. The analysis is carried out by means of the first method of Liapunov. The results are somewhat modified, however, to obtain greater generality without which the technique is too laborious to be useful.
Dynamic Stability of a Pendulous Missile Suspension System
Engineering Mechanics Department, Space Technology Laboratories, Inc., Los Angeles, Calif.
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Chobotov, V. (June 1, 1962). "Dynamic Stability of a Pendulous Missile Suspension System." ASME. J. Appl. Mech. June 1962; 29(2): 276–282. https://doi.org/10.1115/1.3640541
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