Use this URL to cite or link to this record in EThOS: http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560732
Title: Robust control of high altitude long endurance unmanned aerial vehicles using novel lift effectors
Author: Cook, Robert Graham
Awarding Body: Imperial College London
Current Institution: Imperial College London
Date of Award: 2012
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Abstract:
High-Altitude Long-Endurance Unmanned Aerial Vehicles (HALE UAVs) have been the focus for many researchers in the past decades, and are becoming more and more attainable as technology is improving. Recent interest into solar-powered HALE UAVs is leading the way to achieving flight-times which are not limited by a requirement for refuelling, and could continue for months at a time. Such aircraft have huge potential in providing reconnaissance or communications services, and could potentially take on the usual roles of satellites as a much cheaper alternative. One area of HALE UAV design which requires further technological developments is automated control of trajectory, and active alleviation of gusts. The latter concern is of particular interest to this thesis. In this work, a coupled flight dynamics and aeroelastic methodology will be introduced. This approach features a geometrically-exact beam model, which is required to capture the large deformations expected in such flexible aircraft, along with unsteady aerodynamics. The intrinsically nonlinear system is then linearised to provide an approximation to the system dynamics which is more approachable for control synthesis. With a linearisation of the system, robust linear control methods are applied to derive a controller which can reduce the loading onto the system, while simultaneously stabilising it and providing some degree of robustness which can still perform given the unmodelled dynamics that appear in the nonlinear system. This linear control approach will be investigated on two types of HALE UAV with very different dynamic responses to determine how well such control methods deal with nonlinearities, and what the limitations of such an approach may be to apply in real-life. In addition, various novel control effectors will be then considered for gust alleviation of a very flexible aircraft, using the closed-loop control as a method to fairly assess their effectiveness.
Supervisor: Palacios Nieto, Rafael Sponsor: Engineering and Physical Sciences Research Council ; QinetiQ (Firm)
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID: uk.bl.ethos.560732  DOI: Not available
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