Please use this identifier to cite or link to this item:
|Title:||Modelling and robust control of fluidic thrust vectoring and circulation control for unmanned air vehicles.|
|Publisher:||Professional Engineering Publishing.|
|Citation:||Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2008, 222 (5), pp. 333-345.|
|Abstract:||This paper presents actuator models for fluidic thrust vectoring and circulation control and they are used in the design of a robust controller for an unmanned air vehicle. The pitching and rolling moments for the aircraft are produced through the use of a co-flow fluidic thrust vectoring arrangement at the wing trailing edges. Experimental results for the co-flow actuators are used to derive mathematical models and their performance is compared with conventional control surfaces. For the controller design, nonlinear dynamic models are approximated by a simplified linear parameter varying (LPV) model. The polytopic nature of the controller is exploited to reformulate the LPV controller design problem into a m-synthesis problem. The LPV controllers exhibit superior stability properties over the entire operating region, when compared to conventional gain-scheduling schemes.|
|Rights:||This is the final published version of the paper that was first published as, Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2008, 222 (5), pp. 333-345. This version can be found at http://www.pepublishing.com/, Doi: 10.1243/09596518JSCE485.|
|Appears in Collections:||Published Articles, Dept. of Engineering|
Items in LRA are protected by copyright, with all rights reserved, unless otherwise indicated.