DocumentCode :
3213982
Title :
Optimization design of the ship-borne warning helicopter guided missile attack search parameters optimization
Author :
Zhang Lin ; Ma Liang
Author_Institution :
Dept. of Missile, Dalian Naval Acad., Dalian, China
fYear :
2015
fDate :
23-25 May 2015
Firstpage :
1940
Lastpage :
1945
Abstract :
Ship-borne warning helicopter in the search target process need to determine load machine search height and airborne radar beam Angle of pitch. Based on airborne radar search principle, the establishment of radar load perception area model, combined arms constraint sure to meet the requirements of search parameters. Considering the largest airborne radar search distance and target cumulative detection probability, establish airborne radar detection probability model to satisfy the detection probability given the circumstances, to get to the maximum detection range of an attack according to the search parameters the ship-borne warning helicopter flight height and beam Angle of pitch range. And gives the flight altitude and optic axis dip Angle range of use and control method.
Keywords :
airborne radar; helicopters; military radar; missile guidance; probability; radar detection; airborne radar beam angle of pitch; airborne radar detection probability model; airborne radar search distance; airborne radar search principle; arms constraint; flight altitude; load machine search height; optic axis dip angle range; radar load perception area model; search target process; ship-borne warning helicopter guided missile attack search parameter optimization design; target cumulative detection probability; Airborne radar; Atmospheric modeling; Helicopters; Load modeling; Radar antennas; Radar detection; Optimization design; Search parameters; Ship-borne warning helicopter;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location :
Qingdao
Print_ISBN :
978-1-4799-7016-2
Type :
conf
DOI :
10.1109/CCDC.2015.7162237
Filename :
7162237
Link To Document :
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