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NASA NTRS · 19890043443

Model reduction for flexible space structures

Abstract

This paper presents the conditions under which modal truncation yields a near-optimal reduced-order model for a flexible structure. Next, a robust model reduction technique to cope with the damping uncertainties typical of flexible space structure is developed. Finally, a flexible truss and the COFS-1 structure are used to give realistic applications for the model reduction techniques studied in the paper.

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BibTeXRIS

Gawronski, Wodek, Williams, Trevor. 1989-01-01. Model reduction for flexible space structures. https://ntrs.nasa.gov/citations/19890043443

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