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.]