Aircraft load alleviation by specifying its closed-loop eigenstructure

2018-03-26T14:08:48Z (GMT) by Qazi R. Ali
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.]

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CC BY-NC-ND 4.0