DocumentCode
2524268
Title
Derivation and simulation of three dimensional guidance law
Author
Liu, Zhiping ; Chen, Guoshao
Author_Institution
Sch. of Comput. Sci. & Eng., Xi´´an Technol. Univ., Xi´´an, China
fYear
2011
fDate
23-25 May 2011
Firstpage
3803
Lastpage
3807
Abstract
In this paper, three dimensional guidance law was proposed. It differs from previous guidance laws in three aspects, considering the random maneuverability of target, considering the relative acceleration along the line of sight, considering the difference between the commanded acceleration and realistic acceleration of missile. The derivation of three dimensional guidance law was derived based on sliding mode control theory, the effectiveness of the derived guidance laws was validated through the three dimensional simulation, the future research work was also recommended finally.
Keywords
missile guidance; variable structure systems; missile; random maneuverability; sliding mode control theory; three dimensional guidance law; three dimensional simulation; Acceleration; Aerodynamics; Equations; Mathematical model; Missiles; Solid modeling; Target tracking; Guidance Law; Maneuverability; Sliding Mode Control; three dimensional tracking;
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.2011.5968886
Filename
5968886
Link To Document