Efficency Evaluation for Aircraft under Reconfiguration Control Subtitle as Needed

Article Preview

Abstract:

Advanced flighter has many control surfaces.Because that reconfiguration technique can be used to retain a sufficient level of flying quality to enable a surface failure aircraft to safety.At the same time the control efficiency change.The estimate algorithm is used to evaluate the control efficency.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 562-564)

Pages:

865-871

Citation:

Online since:

August 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Su Haoqin, Deng Jianhua1, Ge Tong. Journal of Northwestern Polytechnical U niversity[J]. On Explor ing Ef fect ive Deploymen t of Large Number of Control Surfaces of Advanced Fighter. 2003. 12. Vol21(6).

Google Scholar

[2] Kemin Zhou, Phalguna K Rachinayani, Nike Liu, Zhang Ren, and Jorge Aravena. Fault Diagnosis and Reconfigurable Control For Flight Control System with Actuator Failures. 43rd IEEE Conference on Decision and Control. December 14-17, 2004, pp.1-11.

DOI: 10.1109/cdc.2004.1429644

Google Scholar

[3] Professor D. Mclean,S. Aslam-Mir H Fault Detection AND Control Reconfiguration in flight control.

Google Scholar

[4] Shao Hua-zhang , Yang Zhen-yu, Chen Zong-j i. Control and Decision[J]. Aplication of Pseudo-Inverse Methodto Flight Conrol Reconf iguration. 1999. 5, Vol14(3).

Google Scholar

[5] Zhang Ming-lian. Flight Control System[M]. Beijing. Navigation Industry Press. (1993).

Google Scholar

[6] ZHAN Zheng-yong , LIU-Lin. Implementation of Control Distribution in Flight Control with Multi-Effectors[J] . 2006. 07, Vol24(2). Figure 3. Signals from system with control distribution module under failure.

Google Scholar