Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/111538
Title: An Optimization Approach to Integrated Aircraft-Controller Design
Authors: Yang, G.-H. 
Lum, K.-Y. 
Keywords: Aircraft design
Control surfaces
H∞ control
Linear matrix inequalities (LMIs)
Linear systems
Optimization
Issue Date: 2003
Citation: Yang, G.-H.,Lum, K.-Y. (2003). An Optimization Approach to Integrated Aircraft-Controller Design. Proceedings of the American Control Conference 2 : 1649-1654. ScholarBank@NUS Repository.
Abstract: This paper is concerned with the problem of optimizing aircraft parameters such as the size of its control surfaces, while meeting closed-loop dynamic performance requirements that are formulated as an optimization problem with matrix inequality constraints. New necessary and sufficient conditions for the solvability of the problem are obtained by introducing extra auxiliary variables. Iterative LMI-based algorithms are developed and applied to the redesign of horizontal tail and spoiler for the F-4.
Source Title: Proceedings of the American Control Conference
URI: http://scholarbank.nus.edu.sg/handle/10635/111538
ISSN: 07431619
Appears in Collections:Staff Publications

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