DocumentCode :
1684489
Title :
Optimal antenna pattern design for platform motion compensation
Author :
Ren, Y. ; Peng, Y.N.
Author_Institution :
Beijing Univ., China
fYear :
1998
Firstpage :
343
Lastpage :
348
Abstract :
Auxiliary array patterns in conjunction with the primary receive pattern are widely used for platform motion compensation in airborne and heliborne radar systems. An improved approach for radar auxiliary antenna design is presented. Two corresponding correction patterns of an arbitrary receive pattern are derived under a new criterion, in which the minimization of the total clutter residue averaged over all angles needs the least degree of freedom for the array, and therefore, with the possibly surplus degrees of freedom, the sidelobe level of the correction pattern can be further optimized. The results of simulation illustrate that the average clutter cancellation ratio approximates the optimal value and the additional clutter power from the correction patterns is minimized
Keywords :
airborne radar; antenna arrays; antenna radiation patterns; interference suppression; linear antenna arrays; motion compensation; optimisation; radar antennas; radar clutter; radar detection; receiving antennas; search radar; airborne radar systems; angles; auxiliary array patterns; average clutter cancellation ratio; clutter power; correction patterns; degrees of freedom; heliborne radar systems; linear array; moving target detection; optimal antenna pattern design; platform motion compensation; primary receive pattern; radar auxiliary antenna design; sidelobe level; simulation; surveillance radar; total clutter residue minimization; Airborne radar; Azimuth; Clutter; Doppler radar; Doppler shift; Jamming; Military computing; Motion compensation; Phased arrays; Radar antennas;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Radar Conference, 1998. RADARCON 98. Proceedings of the 1998 IEEE
Conference_Location :
Dallas, TX
Print_ISBN :
0-7803-4492-8
Type :
conf
DOI :
10.1109/NRC.1998.678025
Filename :
678025
Link To Document :
بازگشت