DocumentCode
2258004
Title
Integrated missile guidance and control design with smooth adaptive sliding mode control
Author
Jialing, Zhou ; Jianying, Yang
Author_Institution
State Key Laboratory for Turbulence and Complex Systems, Department of Mechanics and Engineering Science, College of Engineering, Peking University, Beijing 100871, P.R. China
fYear
2015
fDate
28-30 July 2015
Firstpage
5206
Lastpage
5211
Abstract
This paper considers the problem of a missile intercepting a maneuvering target with demand for fast finite-time convergence and anti-chattering. Based on the widely used proportional navigation strategy, a novel integrated guidance and control (IGC) scheme is proposed, which is formulated as a second-order affine nonlinear system with uncertainties. Then the smooth adaptive nonsingular terminal sliding mode control (SANTSMC) method which is proposed in our pervious work is applied to this IGC scheme. By virtue of the SANTSMC method, the uncertainties with unknown bounds can be addressed, fast finite-time convergence can be achieved, and the chattering problem can be well solved.
Keywords
Acceleration; Adaptive systems; Conferences; Missiles; Navigation; Sliding mode control; Uncertainty; Adaptive Sliding Mode Control; Anti-chattering; Integrated Guidance and Control; Missile Interception;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7260451
Filename
7260451
Link To Document