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