Aircraft load alleviation by specifying its closed-loop eigenstructure
thesisposted on 26.03.2018 by Qazi R. Ali
In order to distinguish essays and pre-prints from academic theses, we have a separate category. These are often much longer text based documents than a paper.
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.]
- Aeronautical, Automotive, Chemical and Materials Engineering
- Aeronautical and Automotive Engineering