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