Nutation of a Free Gyro Subjected to an Impulse

Author:

Plymale B. T.1,Goodstein R.1

Affiliation:

1. Boeing Airplane Company, Seattle, Wash.

Abstract

Abstract It is the purpose of this paper to call attention to a particular gyro motion which has been observed and studied in our laboratories. The phenomenon is of extreme practical importance for all instruments which use a gyro as a space-stable element, and no published usable information has been found concerning it. A description and explanation of the motion will be presented. An Appendix contains the basic equations for the system and the results of approximate solutions.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Mechanics of Multi-body Systems;Dynamical Problems of Rigid-Elastic Systems and Structures;1991

2. On Mechanics of Gyroscopes in Gimbal Suspension;Dynamics of Multibody Systems;1978

3. Kinematical Drift of two Degree of Freedom Gyroscopes;ZAMM - Zeitschrift für Angewandte Mathematik und Mechanik;1974

4. On the dynamics of a system of rigid bodies;Theoretical and Applied Mechanics;1973

5. Inertial navigation;Journal of the Franklin Institute;1958-11

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