TY - GEN
T1 - Reconfigurable flight control system design using eigenstructure assignment and particle swarm optimization algorithm
AU - Zhang, Meng
AU - Zhang, Weiguo
AU - Sun, Yong
AU - Ning, Ning
PY - 2010
Y1 - 2010
N2 - 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.
AB - 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.
KW - Constrained output feedback
KW - Eigenstructure assignment
KW - Particle swarm optimization
KW - Reconfigurable flight control system
UR - http://www.scopus.com/inward/record.url?scp=77957942352&partnerID=8YFLogxK
U2 - 10.1109/ICACC.2010.5486839
DO - 10.1109/ICACC.2010.5486839
M3 - 会议稿件
AN - SCOPUS:77957942352
SN - 9781424458462
T3 - Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010
SP - 362
EP - 366
BT - Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010
T2 - 2010 IEEE International Conference on Advanced Computer Control, ICACC 2010
Y2 - 27 March 2010 through 29 March 2010
ER -