DocumentCode :
3112133
Title :
A linearized model for the line of sight guidance law
Author :
Belkhouche, E. ; Belkhouche, B. ; Rastgoufard, P.
Author_Institution :
Electr. Eng. & Comput. Sci. Dept., Tulane Univ., New Orleans, LA, USA
fYear :
2004
fDate :
26-29 April 2004
Firstpage :
201
Lastpage :
207
Abstract :
This paper deals with the linearization of the nonlinear model describing the kinematics equations of the line of sight guidance law. The linearized model is derived based on optimization techniques, where different cost functions are used. It turns out that in the case of maneuvering targets, the linear coefficients are time independent and time dependent in the case of maneuvering targets. In both cases these coefficients depend on the initial line of sight angle, which means that the linearization has the same order as the nonlinear system. The linearization method is illustrated using simulation, and a comparison with the classical linearization is provided.
Keywords :
missile guidance; navigation; cost functions; kinematics equations; line of sight guidance law; linear coefficients; linearized model; nonlinear model; optimization techniques; Aerodynamics; Cost function; Game theory; Kinematics; Modems; Motion control; Nonlinear equations; Nonlinear systems; Optimal control; Process control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Position Location and Navigation Symposium, 2004. PLANS 2004
Print_ISBN :
0-7803-8416-4
Type :
conf
DOI :
10.1109/PLANS.2004.1308994
Filename :
1308994
Link To Document :
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