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Technical Briefs

Partial Stabilization Approach to 3-Dimensional Guidance Law Design

[+] Author and Article Information
T. Binazadeh

 School of Electrical and Electronic Engineering, Shiraz University of Technology, Shiraz, Iranbinazadeh@sutech.ac.ir

M. J. Yazdanpanah

 Control & Intelligent Processing Center of Excellence, School of Electrical and Computer Engineering, University of Tehran, P.O. Box 14395/515, Tehran, Iranyazdan@ut.ac.ir

J. Dyn. Sys., Meas., Control 133(6), 064504 (Nov 22, 2011) (4 pages) doi:10.1115/1.4004575 History: Received March 19, 2010; Revised April 16, 2011; Published November 22, 2011; Online November 22, 2011

In this paper, a new approach to design the 3-dimensional missile guidance law, based on partial stabilization, is presented. The approach is based on the classification of the state variables within the guidance system dynamics with respect to their required stabilization properties. The resulting guidance law enables the missile to intercept highly maneuvering targets within a finite interception time. Effectiveness of the proposed guidance law is demonstrated through analysis and simulations.

FIGURES IN THIS ARTICLE
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Copyright © 2011 by American Society of Mechanical Engineers
Topics: Stability , Design , Missiles
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Figures

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Figure 1

3-dimensional missile-target geometry

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Figure 2

Trajectories of the missile and the target

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Figure 3

(a) Radial guidance command (ur) (b) tangential guidance command (uθ), and (c) tangential guidance command (uϕ)

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