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Title: Aircraft load alleviation by specifying its closed-loop eigenstructure
Author: Ali, Qazi R.
ISNI:       0000 0001 3413 6078
Awarding Body: Loughborough University of Technology
Current Institution: Loughborough University
Date of Award: 1987
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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:  DOI: Not available
Keywords: Aircraft load control system