Title :
A study of chattering suppression in sliding mode-based missile guidance law
Author :
Yuan Liying ; Wu Junfeng ; Yu Lianyong ; Cui Jiashan ; Sun Lili
Author_Institution :
Sch. of Autom., Harbin Univ. of Sci. & Technol., Harbin, China
Abstract :
A sliding mode controller with chattering suppression for missiles guidance law is designed under the presence of target maneuvering. To reduce the chattering in sliding mode control, constitute a continuous function instead of signal function which guarantees the practicability of the control scheme. In the numerical simulation, it is obviously that the proposed guidance law reduces the chattering phenomenon and.
Keywords :
military systems; missile guidance; target tracking; variable structure systems; chattering suppression; signal function; sliding mode based missile guidance law; sliding mode control; target maneuvering; Azimuth; Robustness; Missile; guidance law; maneuvering target; sliding mode control;
Conference_Titel :
Strategic Technology (IFOST), 2011 6th International Forum on
Conference_Location :
Harbin, Heilongjiang
Print_ISBN :
978-1-4577-0398-0
DOI :
10.1109/IFOST.2011.6021171
