Natesan, Kannan, Gu, Da-Wei and Postlethwaite, Ian (2010) Design of linear parameter varying trajectory tracking controllers for an unmanned air vehicle. Journal of Aerospace Engineering, 224 (4). pp. 395-402. ISSN 0954-4100
Full text not available from this repository. (Request a copy)Abstract
This article presents a trajectory tracking controller design approach for an unmanned air vehicle using the linear parameter varying (LPV) methods. The longitudinal and lateral controllers are designed using an inner-outer loop structure with the inner loop LPV controller designed first using μ-synthesis. The inner loop is then approximated with a reference model and the outer loop is designed using loop-shaping techniques. Flight trajectory is expressed in terms of earth co-ordinates, which the outer loop controller converts into reference signals for the inner loop. Full-scale non-linear simulations are used to test the efficiency of the designed controller and of the proposed design approach.
Item Type: | Article |
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Uncontrolled Keywords: | flight control, linear parameter varying systems, robust control, unmanned air vehicle |
Subjects: | H400 Aerospace Engineering |
Department: | Faculties > Engineering and Environment > Mathematics, Physics and Electrical Engineering |
Depositing User: | Katie Harwood |
Date Deposited: | 03 Jan 2013 11:30 |
Last Modified: | 13 Oct 2019 00:30 |
URI: | http://nrl.northumbria.ac.uk/id/eprint/10926 |
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