Return to search

Aircraft load alleviation by specifying its closed-loop eigenstructure

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.

Identiferoai:union.ndltd.org:bl.uk/oai:ethos.bl.uk:376800
Date January 1987
CreatorsAli, Qazi R.
PublisherLoughborough University
Source SetsEthos UK
Detected LanguageEnglish
TypeElectronic Thesis or Dissertation
Sourcehttps://dspace.lboro.ac.uk/2134/32363

Page generated in 0.0018 seconds