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NASA NTRS · 19830027807

Large space structure model reduction and control system design based upon actuator and sensor influence functions

Abstract

A model reduction procedure based on aggregation with respect to sensor and actuator influences rather than modes is presented for large systems of coupled second-order differential equations. Perturbation expressions which can predict the effects of spillover on both the aggregated and residual states are derived. These expressions lead to the development of control system design constraints which are sufficient to guarantee, to within the validity of the perturbations, that the residual states are not destabilized by control systems designed from the reduced model. A numerical example is provided to illustrate the application of the aggregation and control system design method.

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Yam, Y., Lang, J. H., Johnson, T. L., Shih, S., Staelin, D. H.. 1983-07-01. Large space structure model reduction and control system design based upon actuator and sensor influence functions. https://ntrs.nasa.gov/citations/19830027807

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