NDLI: Application of gain scheduled eigenstructure assignment to flight control design

Content Provider	IEEE Xplore Digital Library
Author	Piou, J.E. Sobel, K.M.
Copyright Year	1996
Description	Author affiliation: Lincoln Lab., MIT, Lexington, MA, USA (Piou, J.E.)
Abstract	Eigenstructure assignment is a method which allows the incorporation of classical specifications on damping, settling time, and mode decoupling into a modern multivariable control framework. This method allows the designer to directly satisfy damping, settling time, and mode decoupling specifications by directly choosing the eigenvalues and eigenvectors. In this paper, we combine eigenstructure assignment with gain scheduling to obtain an algorithm which does not require the non-singularity of a matrix at a particular value of the parameter. The eigenstructure assignment gain scheduling computation is a direct non-iterative expression for the plant which was considered by Shahruz and Behtash (1992). For each value of the parameter the gain expression is a natural extension of the gain computation for the standard linear plant which was considered by Sobel et al. (1989).
Starting Page	101
Ending Page	106
File Size	495883
Page Count	6
File Format	PDF
ISBN	0780329759
DOI	10.1109/CCA.1996.558614
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1996-09-15
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Aerospace control Control systems Processor scheduling Eigenvalues and eigenfunctions Output feedback Equations Damping Design methodology Scheduling algorithm MIMO
Content Type	Text
Resource Type	Article

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