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
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