Thesis-1987-Ali.pdf (5.11 MB)
Aircraft load alleviation by specifying its closed-loop eigenstructure
thesis
posted on 2018-03-26, 14:08 authored by Qazi R. AliReduction 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. [Continues.]
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Publisher
© Qazi Rashid AliPublisher statement
This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/Publication date
1987Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy at Loughborough University.Language
- en