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Mixed sensitivity design: An aerospace case study
World Congress, Volume # 15 | Part# 1
Location: , Barcelona, Spain
National Organizing Committee Chair: Gabriel Ferraté,
Eduardo F. Camacho
International Program Committee Chair: Luis Basañez,
Juan A. de la Puente
Conference Editor: Luis Basañez,
Juan A. de la Puente
Authors
Huibert Kwakernaak
Digital Object Identifier (DOI)
10.3182/20020721-6-ES-1901.01234
Page Numbers:
1232-1232
Index Terms
mixed sensitivity design,stability augmentation system,H˞ optimization,H2 optimization
Abstract
The mixed sensitivity design method for multivariable linear control systems proposed in the companion paper (Kwakernaak, 2001) is applied to the design of a stability augmentation system for the longitudinal motion of a fighter airplane previously studied by Safonov and Chiang (1988). Both H∞ and H2 mixed sensitivity design are considered. They lead to quite similar results.
References
[1] M. G. Safonov and R. Y. Chiang (1988), "CACSD
using the state-space L∞ theory - A design example,"
IEEE Trans. Aut. Control 33, pp. 477-
479.
[2] R. Y. Chiang and M. G. Safonov (1988), Robust-Control
Toolbox User's Guide, The MathWorks,
S. Natick, MA, USA.
[3] H. Kwakernaak (2001), "Mixed sensitivity design,"
submitted for presentation during the 15th IFAC
World Congress, July 21-26, 2002, Barcelona,
Spain.
[4] B. L. Stevens and F. L. Lewis (1992), Aircraft control
and simulation. John Wiley & Sons, Inc.