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NASA NTRS · 19800056578

Optimal member damper controller design for large space structures

Abstract

Consideration is given to the selection of velocity feedback gains for individual dampers for the members of a structurally controlled large flexible space structure. The problem is formulated as an optimal output feedback regulator problem, and necessary conditions are derived for minimizing a quadratic performance function. The diagonal nature of the gain matrix is taken into account, along with knowledge of noise covariances. It is pointed out that the method presented offers a systematic approach to the design of a class of controllers for enhancing structural damping, which have significant potential if used in conjunction with a reduced-order optimal controller for rigid-body modes and selected structural modes.

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BibTeXRIS

Joshi, S. M., Groom, N. J.. 1980-08-01. Optimal member damper controller design for large space structures. https://ntrs.nasa.gov/citations/19800056578

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