Open-Loop Resonance-Cancellation Control for a Base-Excited Pendulum

Author:

Soper R. Randall1,Lacarbonara Walter2,Chin Char-Ming3,Nayfeh Ali H.4,Mook Dean T.4

Affiliation:

1. Department of Mechanical Engineering, Tennessee Technical University, PO. Box 5014, Cookeville, TN 38505, USA

2. Dipartimento di Ingegneria Strutturale e Geotecnica, Universita di Roma "La Sapienza," via Eudossiana 18, 00184 Roma, Italy

3. VSAS GPC, General Motors Corp., MC 480-305-200, 6440 E 12 Mile Road, Warren, MI48090-9000, USA

4. Department of Engineering Science and Mechanics, MC 0219, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061, USA

Abstract

A new open-loop control strategy applied to a planar pendulum subjected to the most severe com bination of base excitations, horizontal motion at the primary-resonance frequency, and vertical motion at the principal-parametric resonance frequency is developed. The control action is typical of many single-input control systems; the control authority in one direction (horizontal) is high, and the control authority in the or thogonal direction (vertical) is zero in a linear sense. Although the action of the controller is linearly orthog onal to part (vertical or parametric) of the system excitation, effects are transferred to this direction through nonlinear actuator action. Proper enhancement of the control input allows the nonlinear action to provide con trol authority over the parametric excitation. The dynamics at reduced orders, determined by a multiple-scales perturbation analysis, suggest the appropriate form for the control enhancement. The normal form of the sys tem provides information about how each parameter of the enhancement affects the steady-state pendulation of the system. In this case, heuristic arguments are used to reduce the dimension of the unknown enhance ment design parameters to a manageable size. The maximum pendulation angle of the steady-state motion of the system is one of the appropriate metrics for the system response; here it is used as the cost function for evaluation of the optimal enhancement gains. Because the size of the design parameter set has been re duced, a simple grid search is employed to find the optimal control. Relative to simple linear cancellation of the disturbance, the proposed approach reduces the response of the system by an order of magnitude for typical disturbance cases.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering,Automotive Engineering,General Materials Science

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