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Spillover, nonlinearity, and flexible structuresMany systems whose evolution in time is governed by Partial Differential Equations (PDEs) are linearized around a known equilibrium before Computer Aided Control Engineering (CACE) is considered. In this case, there are infinitely many independent vibrational modes, and it is intuitively evident on physical grounds that infinitely many actuators would be needed in order to control all modes. A more precise, general formulation of this grave difficulty (spillover problem) is due to A.V. Balakrishnan. A possible route to circumvention of this difficulty lies in leaving the PDE in its original nonlinear form, and adding the essentially finite dimensional control action prior to linearization. One possibly applicable technique is the Liapunov Schmidt rigorous reduction of singular infinite dimensional implicit function problems to finite dimensional implicit function problems. Omitting details of Banach space rigor, the formalities of this approach are given.
Document ID
19910012995
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bass, Robert W.
(Rockwell International Science Center Thousand Oaks, CA., United States)
Zes, Dean
(McDonnell-Douglas Helicopter Co. Mesa, AZ., United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA. Langley Research Center, Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N22308
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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