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 |
Show full item record
Files in This Item:
There are no files associated with this item.
Google ScholarTM
Check
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.