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Positive position feedback control for large space structures

AIAA Journal · 1990 · Vol. 28(4) · pp. 717–724
James L. FansonT. K. Caughey

Abstract

A new technique for vibration suppression in large space structures is investigated in laboratory experiments on a thin cantilever beam. This technique, called Positive Position Feedback, makes use of generalized displacement measurements to accomplish vibration suppression. Several features of Positive Position Feedback make it attractive for the large space structure control environment: The realization of the controller is simple and straightforward. Global stability conditions can be derived which are independent of the dynamical characteristics of the structure being controlled, i.e., all spillover is stabilizing. The method cannot be destabilized by finite actuator dynamics, and the technique is amenable to a strain-based sensing approach. The experiments control the first six bending modes of a cantilever beam, and make use of piezoelectric materials for actuators and sensors, simulating a piezoelectric active-member. The modal damping ratios are increased by factors ranging from 2 to 130.

Aeroelasticity and Vibration ControlDynamics and Control of Mechanical SystemsVibration Control and Rheological FluidsCantileverControl theory (sociology)ActuatorVibration controlPosition (finance)Displacement (psychology)VibrationActive vibration controlBeam (structure)Realization (probability)

Funding

  • National Aeronautics and Space Administration
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