DocumentCode
2525790
Title
Three dimensional tracking guidance law for guided munitions
Author
Liu, Zhiping ; Yu, Fan
Author_Institution
Sch. of Comput. Sci. & Eng., Xi´´an Technol. Univ., Xian, China
fYear
2011
fDate
23-25 May 2011
Firstpage
4248
Lastpage
4252
Abstract
In this paper, three dimensional guidance (3-D) law is derived based on the variable structure control (VSC) theory for the spatial tracking and attacking. Moreover the relationship between the measurement error and guidance error is investigated and discussed thoroughly. The 3-D guidance law based on VSC is modified in order to be implemented simply. The performance of modified guidance law is verified through the comparison compared with traditional guidance law based on the computer simulation.
Keywords
missile guidance; position control; variable structure systems; 3D guidance law; VSC theory; spatial tracking; three dimensional tracking guidance law; variable structure control theory; Acceleration; Equations; Mathematical model; Measurement errors; Missiles; Uncertainty; 3-Dguidance law; Guidance error; Measurement error; Variable structure control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2011 Chinese
Conference_Location
Mianyang
Print_ISBN
978-1-4244-8737-0
Type
conf
DOI
10.1109/CCDC.2011.5968972
Filename
5968972
Link To Document