Abstract
EXTENDED ABSTRACT Future mission requirements will undoubtedly require increasingly larger, more complex spacecraft. As spacecraft become larger, the effects of structural flexibility and dynamic coupling impose additional requirements on the control system design. This paper describes a series of efficient computational tools developed to perform stability analyses on multi-input/multi-output linear systems of relatively high order. The software package is designed around a collection of efficient, reliable routines (References 1 and 2) to compute eigenvalues and eigenvectors, Hessenberg and QR transformations, and singular value decomposition. These routines have been written to be highly space and time efficient and, in general, allow most analyses to be performed in an interactive timesharing environment.
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