2134/32363
Qazi R. Ali
Qazi R.
Ali
Aircraft load alleviation by specifying its closed-loop eigenstructure
Loughborough University
2018
untagged
Engineering not elsewhere classified
2018-03-26 14:08:48
Thesis
https://repository.lboro.ac.uk/articles/thesis/Aircraft_load_alleviation_by_specifying_its_closed-loop_eigenstructure/9217118
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. [Continues.]