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NASA NTRS · 19890024319

Analysis of limit cycles in control systems for joint dominated structures

Abstract

An approach to the modeling of limit cycles due to joint nonlinearities in large joint dominated space structures is presented which makes it possible to predict limit cycles and determine their stability. An actively controlled truss structure with nonlinear joints is modeled as a linear system with nonlinear feedback by separating the joint load-displacement characteristics into a linear part, which prevails at large displacements, and a nonlinear part. By replacing the joints by their linear parts, it is possible to perform a standard model decomposition which yields a reduced order linear model. Linear control laws can be easily included into the linear part of the system; nonlinear control laws can be implemented but they must be fed back to the linear model. The modeling approach described here allows straightforward limit cycle analysis.

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BibTeXRIS

Mercadal, M., Vander Velde, W. E.. 1988-01-01. Analysis of limit cycles in control systems for joint dominated structures. https://ntrs.nasa.gov/citations/19890024319

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