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Gain weighted eigenspace assignmentThis report presents the development of the gain weighted eigenspace assignment methodology. This provides a designer with a systematic methodology for trading off eigenvector placement versus gain magnitudes, while still maintaining desired closed-loop eigenvalue locations. This is accomplished by forming a cost function composed of a scalar measure of error between desired and achievable eigenvectors and a scalar measure of gain magnitude, determining analytical expressions for the gradients, and solving for the optimal solution by numerical iteration. For this development the scalar measure of gain magnitude is chosen to be a weighted sum of the squares of all the individual elements of the feedback gain matrix. An example is presented to demonstrate the method. In this example, solutions yielding achievable eigenvectors close to the desired eigenvectors are obtained with significant reductions in gain magnitude compared to a solution obtained using a previously developed eigenspace (eigenstructure) assignment method.
Document ID
19940032313
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Davidson, John B.
(NASA Langley Research Center Hampton, VA, United States)
Andrisani, Dominick, II
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-109130
NAS 1.15:109130
Report Number: NASA-TM-109130
Report Number: NAS 1.15:109130
Accession Number
94N36820
Funding Number(s)
PROJECT: RTOP 505-64-30-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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