Use this URL to cite or link to this record in EThOS: http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.275481
Title: Robust control of systems subject to input non-linearities with application to high performance helicopters
Author: Turner, Matthew Christopher
ISNI:       0000 0001 2448 8416
Awarding Body: University of Leicester
Current Institution: University of Leicester
Date of Award: 2000
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Abstract:
This thesis addresses some of the issues associated with linear systems subject to nonlinearities at their input, and considers robust control of high performance helicopters. In particular, the problems of substitution and saturation nonlinearities are discussed. In the case of the former, a new procedure based on ideas from optimal control is developed to help facilitate dynamic transfer between two linear controllers. For the latter, a generalisation of an existing scheme is made which allows asymptotic set-point tracking for all states belonging to a given subset of the state space. The closely related problem of limited authority control is considered and promising results are demonstrated on the Westland Lynx helicopter in a pilotted simulation. The thesis culminates with a discussion of the design and implementation of an Hinfinity controller for the Bell 205 helicopter. The results show that in flight, the helicopter attained good handling qualities ratings, even though the fidelity of some of the mathematical models was relatively low.
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID: uk.bl.ethos.275481  DOI: Not available
Keywords: Control systems & control theory Automatic control Control theory Aeronautical instruments
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