Published June 2005
| Version public
Book Section - Chapter
Robust Stability and Performance Analysis of a Longitudinal Aircraft Model Using Sum of Squares Techniques
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1.
California Institute of Technology
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2.
University of Cambridge
Abstract
In this paper we demonstrate how the recently developed sum of squares techniques can be used to analyze robust stability and robust performance of quasi-LPV models. We show the effectiveness of the methodology through the analysis of the stability and performance of a nonlinear control law applied to an uncertain quasi-LPV model of the short-period dynamics of an F/A-18 aircraft
Additional Information
© 2005 IEEE. Date of Current Version: 13 March 2006. The second author would like to acknowledge the help of Dr. Yoge Patel and Ian Kaynes from QinetiQ Ltd for providing the software and technical documentation for the nonlinear, aeroservoelastic F/A-18 model.Additional details
Identifiers
- Eprint ID
- 25091
- DOI
- 10.1109/.2005.1467199
- Resolver ID
- CaltechAUTHORS:20110825-103014156
Dates
- Created
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2011-08-25Created from EPrint's datestamp field
- Updated
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2021-11-09Created from EPrint's last_modified field
Caltech Custom Metadata
- Other Numbering System Name
- INSPEC Accession Number
- Other Numbering System Identifier
- 8688288