By Topic

Reconfigurable flight control system design using eigenstructure assignment and particle swarm optimization algorithm

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

4 Author(s)
Meng Zhang ; Coll. of Autom., Northwestern Polytech. Univ., Xi''an, China ; Weiguo Zhang ; Yong Sun ; Ning Ning

This paper proposes a new reconfigurable flight control system design methodology using the optimal eigenstructure assignment with constrained output feedback. An integrated performance index is given in this methodology which combines the performance index of the reconfigured eigenstructure and the performance index of the stability of the reconfigured closed-loop system. Then particle swarm optimization algorithm is utilized to minimize the integrated performance index to obtain the optimal feedback gain. In view of an impaired lateral flight control system with the sideslip angle sensor and the aileron are all in complete failure, an illustrative design example using the proposed methodology to design the reconfigurable flight control system. Simulation results are provided to show the effectiveness and the superiority of the proposed methodology.

Published in:

Advanced Computer Control (ICACC), 2010 2nd International Conference on  (Volume:3 )

Date of Conference:

27-29 March 2010