Use this URL to cite or link to this record in EThOS: http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.376800
Title: Aircraft load alleviation by specifying its closed-loop eigenstructure
Author: Ali, Qazi R.
Awarding Body: Loughborough University of Technology
Current Institution: Loughborough University
Date of Award: 1987
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Abstract:
Reduction of aircraft loads, arising as a result of manoeuvre commands or atmospheric turbulence, by means of active control is an important problem in flight control. A variety of methods of designing appropriate control systems to achieve such reduction are available, but not every method is effective. A feature of this research work is the use of an eigenvalue/eigenvector assignment method using full state variable feedback, to design aircraft load alleviation control systems.
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID: uk.bl.ethos.376800  DOI: Not available
Keywords: Aircraft load control system
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