DocumentCode
3585476
Title
Missile Location Based on Missile-Borne Bistatic SAR
Author
Xinqi Fu ; Meirong Chen
Author_Institution
Res. Inst. of Electron. Sci. & Technol., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
Volume
2
fYear
2014
Firstpage
232
Lastpage
235
Abstract
With radar imaging having the characteristics of functioning all-weather, all-day and remote imaging, the using of Synthetic Aperture Radar Seeker is one of the most effective methods to improve the guidance accuracy of medium and long range missile. According to studying the missile positioning method of missile-borne Synthetic Aperture Radar, an integrated missile positioning method based on the Inertial Navigation System and bistatic Synthetic Aperture Radar is proposed in this paper, we can get height information of the missile via an additional antenna system with downward beam. In this paper, the positioning principle is introduced. The method proposed in this paper can get location information of high-speed Synthetic Aperture Radar platform after scene matching with high degree of precision. According to range equation, Doppler equation, the missile speed gained from Inertial Navigation System and the missile altitude measured by altimeter, we can calculate the calculation equation of positioning under the missile-target positioning model which can avoid erratic iteration calculation. Meanwhile, detailed positioning process is proposed in this paper. Simulation results demonstrate that the method proposed in this paper can efficiently meet the positioning requirements of terminal guidance with bistatic missile-borne Synthetic Aperture Radar.
Keywords
Doppler radar; altimeters; height measurement; inertial navigation; missile guidance; missiles; synthetic aperture radar; Doppler equation; altimeter; antenna system; inertial navigation system; integrated missile target positioning method; iteration calculation; missile altitude measurement; missile location; missile-borne bistatic SAR; radar imaging; range equation; remote imaging; synthetic aperture radar seeker; Doppler effect; Mathematical model; Missiles; Projectiles; Receivers; Synthetic aperture radar; Transmitters; inertial navigation system; missile position; missile-borne bistatic SAR;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Intelligence and Design (ISCID), 2014 Seventh International Symposium on
Print_ISBN
978-1-4799-7004-9
Type
conf
DOI
10.1109/ISCID.2014.106
Filename
7081978
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