Title
Research on the Chattering Problem with VSC of Supersonic Missiles Based on Intelligent Materials.
Abstract
Considering pitch channel simplified model of missile control system, a VSCL(variable structure control law) is designed by using overload and angle velocity signals. Especially, an analysis is proposed for the situation of equal control with uncertainties. An integral action is introduced to compensate the uncertainties and a soft function is adopted to solve the chattering problem of VSC. Finally, an analysis for the chattering problem, the function of integral action and soft function is thoroughly studied. The conclusion shows that the dead zone of soft function is a important factor that affect the chattering phenomenon. And the relationship between the chattering problem and the system gain is revealed.
Year
DOI
Venue
2011
10.1007/978-3-642-23321-0_95
ADVANCES IN COMPUTER SCIENCE, ENVIRONMENT, ECOINFORMATICS, AND EDUCATION, PT I
Keywords
Field
DocType
Chattering,VSC,Missile,Uncertain,Stability
Dead zone,Integral action,Computer science,Control theory,Missile,Communication channel,Supersonic speed,Control system,Variable structure control
Conference
Volume
Issue
ISSN
214
PART 1
1865-0929
Citations 
PageRank 
References 
0
0.34
3
Authors
4
Name
Order
Citations
PageRank
Junwei Lei13011.27
Jianhong Shi283.38
Guorong Zhao382.58
Guoqiang Liang462.87