Blending Methodology of Linear Parameter Varying Control Synthesis of F-16 Aircraft System-Reference-Cited by-同舟云学术

Blending Methodology of Linear Parameter Varying Control Synthesis of F-16 Aircraft System

Published:2002-11 Issue:6 Volume:25 Page:1040-1048
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Shin Jong-Yeob¹,Balas Gary J.²,Kaya M. Alpay³

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

2. University of Minnesota, Minneapolis, Minnesota 55455

3. University of California,Berkeley, Berkeley, California 94720

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5008

Reference20 articles.

1. Guaranteed properties of gain scheduled control for linear parameter-varying plants

2. Analysis of gain scheduled control for nonlinear plants

3. Advanced gain-scheduling techniques for uncertain systems

4. 4Becker, G. “Quadratic Stability and Performance of Linear Parameter Dependent Systems,” Ph.D. Dissertation, Dept. of Mechanical Engineering,Univ. of California, Berkeley, CA,1993.

5. 5Wu, F. “Control of Linear Parameter Varying Systems,” Ph.D. Dissertation, Dept. of Mechanical Engineering,Univ. of California, Berkeley, CA,1995.

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