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NASA NTRS · 20010000497

Sliding Mode Control of a Slewing Flexible Beam

Abstract

An output feedback sliding mode controller (SMC) is proposed to minimize the effects of vibrations of slewing flexible manipulators. A spline trajectory is used to generate ideal position and velocity commands. Constrained nonlinear optimization techniques are used to both calibrate nonlinear models and determine optimized gains to produce a rest-to-rest, residual vibration-free maneuver. Vibration-free maneuvers are important for current and future NASA space missions. This study required the development of the nonlinear dynamic system equations of motion; robust control law design; numerical implementation; system identification; and verification using the Sandia National Laboratories flexible robot testbed. Results are shown for a slewing flexible beam.

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BibTeXRIS

Wilson, David G., Parker, Gordon G., Starr, Gregory P., Robinett, Rush D., III. 1997-02-01. Sliding Mode Control of a Slewing Flexible Beam. https://ntrs.nasa.gov/citations/20010000497

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