DocumentCode :
696148
Title :
Capturability of a simple guidance law with angular acceleration input
Author :
Urakubo, Takateru ; Kanade, Takeo
Author_Institution :
Dept. of Comput. Sci. & Syst. Eng., Kobe Univ., Kobe, Japan
fYear :
2009
fDate :
23-26 Aug. 2009
Firstpage :
2390
Lastpage :
2395
Abstract :
This paper examines the capturability of a guidance law that provides a desired angular acceleration of the heading angle to a pursuer. The guidance law has originally been proposed by Fajen and Warren[13], in order to explain the behavior of walking humans. It is shown that the relative rotational motion between a pursuer and an evader can be represented by an equation similar to the equation of motion for a pendulum with a disturbance. A set of sufficient conditions for successful pursuit are derived, and it is proved that the gain parameters of the guidance law can be chosen so that the conditions are satisfied. For sufficiently large gains, a pursuer controlled by the guidance law catches a maneuvering evader while achieving motion camouflage.
Keywords :
missile guidance; motion control; pendulums; angular acceleration input; capturability; evader; guidance law; heading angle; motion camouflage; pendulum; pursuer; relative rotational motion; walking humans; Acceleration; Angular velocity; Equations; Lyapunov methods; Missiles; Trajectory; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 2009 European
Conference_Location :
Budapest
Print_ISBN :
978-3-9524173-9-3
Type :
conf
Filename :
7074763
Link To Document :
بازگشت