DocumentCode :
530604
Title :
Double planes discrete variable structure tracking algorithm
Author :
Li, Zhao-Giang ; Zhou, De-Yun ; Wang, Ling-Xiao ; Xu, Jia-Dong
Author_Institution :
Dept. of Electron. Inf., Northwestern Polytech. Univ., Xian, China
Volume :
4
fYear :
2010
fDate :
24-26 Aug. 2010
Firstpage :
563
Lastpage :
566
Abstract :
With the development of aviation computer and aviation electronics technologies, the analog tracking algorithm has been unable to meet the need in project. But discrete variable structure tracking algorithm meets the requirement. After go into the sliding mode, the traditional discrete variable structure tracking algorithm will take place of buffeting, and will have phenomenon of the exhale when the front angel is big. In light of the above factors, in order to further improve the precision guided, the no buffeting discrete variable structure double planes tracking algorithm with a compensation of the disturbance is given. The simulation results show that the discrete signal guidance law can meet the tactical UCAV indicator.
Keywords :
aerospace control; avionics; discrete systems; variable structure systems; aviation computer; aviation electronics technology; discrete signal guidance law; discrete variable structure; disturbance compensation; double plane tracking algorithm; tactical UCAV indicator; Tracking; discrete signal; double hyperplane; no buffeting; tracking; variable structure control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer, Mechatronics, Control and Electronic Engineering (CMCE), 2010 International Conference on
Conference_Location :
Changchun
Print_ISBN :
978-1-4244-7957-3
Type :
conf
DOI :
10.1109/CMCE.2010.5610070
Filename :
5610070
Link To Document :
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