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
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;
Conference_Titel :
Control and Decision Conference (CCDC), 2011 Chinese
Conference_Location :
Mianyang
Print_ISBN :
978-1-4244-8737-0
DOI :
10.1109/CCDC.2011.5968886
