Affiliation:
1. Department of Mechanical Engineering, University of North Dakota, Grand Forks, ND 58202
2. Department of Mechanical Engineering, University of California at Berkeley, Berkeley, CA 94720
Abstract
The nonlinear integro-differential equations, describing the transverse and rotational motions of a nonuniform Euler-Bernoulli beam with end mass attached to a rigid hub, are derived. The effects of both the linear and nonlinear elastic rotational couplings are investigated. The linear couplings are exactly accounted for in a decoupled Euler-Bernoulli beam model and their effects on the eigensolutions and response are significant for a small ratio of hub-to-beam inertia. The nonlinear couplings with a resultant stiffening effect are negligible for small angular velocities. A discretized model, suitable for the study of large angle, high speed rotation of a nonuniform beam, is presented. The optimal control moment for simultaneous vibration suppression of the beam at the end of a prescribed rotation is determined. Influences of the nonlinearity, nonuniformity, maneuver time, and inertia ratio on the optimal control moment and system response are discussed.
Subject
Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering
Reference16 articles.
1. Akulenko L. D. , and BolotnikN. N., 1983, “On Controlled Rotation of an Elastic Rod,” Journal of Applied Mathematics and Mechanics (PMM), Vol. 46, pp. 465–471.
2. Barbieri E. , and O¨zgu¨nerU¨., 1988, “Unconstrained and Constrained Mode Expansions for a Flexible Slewing Link,” ASME JOURNAL OF DYNAMIC SYSTEMS, MEASUREMENT, AND CONTROL, Vol. 110, pp. 416–421.
3. Cannon R. H. , and SchmitzE., 1985, “Initial Experiments on the End-Point Control of a Flexible One-Link Robot,” The International Journal of Robotics Research, Vol. 3, No. 3, pp. 62–76.
4. Hoa S. V. , 1979, “Vibration of a Rotating Beam with Tip Mass,” Journal of Sound and Vibration, Vol. 67, No. 3, pp. 369–381.
5. Junkins, J. L., and Turner, J. D., 1986, Optimal Spacecraft Rotational Maneuvers, Elsevier Science Publishers B. V., The Netherlands.
Cited by
34 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