DocumentCode :
3135830
Title :
Sliding-mode guidance law based on adaptive observation techniques
Author :
Xu, Zhaoxin ; Hua, Wenhua ; Chen, Xinglin
Author_Institution :
Coll. of Autom., Harbin Eng. Univ., Harbin, China
Volume :
2
fYear :
2011
fDate :
25-28 July 2011
Firstpage :
743
Lastpage :
747
Abstract :
Because some feedback quantities such as high-order line-of-sight rate derivatives are not directly measurable and some inner parameters exist uncertainties, sliding-mode guidance law considering the control loop dynamics goes against the practical application in general. Based on adaptive control and observation techniques, a novel observer-based adaptive sliding-mode guidance law is presented. The observer can realize the on-line estimate of the system states and uncertainties. The nonlinear system simulations show that compared with the traditional proportional navigation and sliding-mode guidance law, provided an enough maneuvering capability exists, this guidance law can not only realize the hit-to-kill of the target, but also has the advantages of maneuvering and homing performance.
Keywords :
adaptive control; feedback; motion control; nonlinear control systems; observers; uncertain systems; variable structure systems; adaptive control; adaptive observation; control loop dynamics; feedback quantity; high-order line-of-sight rate derivatives; homing performance; maneuvering capability; nonlinear system simulation; observer-based adaptive sliding-mode guidance law; proportional navigation; system states; system uncertainty; Acceleration; Adaptive systems; Missiles; Navigation; Observers; Switches; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Information Processing (ICICIP), 2011 2nd International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4577-0813-8
Type :
conf
DOI :
10.1109/ICICIP.2011.6008348
Filename :
6008348
Link To Document :
بازگشت