DocumentCode :
3390682
Title :
Optimal method for interfering with infrared homing missile by airborne infrared smoke
Author :
Tong, Zhongxiang ; Lu, Yanlong ; Li, Chuanliang ; Liu, Pengfei
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an
fYear :
2008
fDate :
10-12 Oct. 2008
Firstpage :
588
Lastpage :
592
Abstract :
As the equipment with high performance-cost ratio, infrared smoke is widely used in the ground infrared countermeasure. But from the air-to-air countermeasure aspect, for the impact of high speed airflow, it is difficult to interfere with the infrared homing missile effectively by the infrared smoke. To overcome this problem, the infrared countermeasure for the complex system which includes combat aircraft target, infrared smoke and infrared homing missile is simulated. Integrating the launching time and initial velocity of the infrared Smoke with the optimal elusion rule of the combat aircraft target, the system simulation not only solves the effect of high speed airflow on the infrared smoke, but also gets the optimal method for interfering with the infrared homing missile by the airborne infrared smoke.
Keywords :
aircraft; electronic countermeasures; jamming; missiles; air-to-air countermeasure; airborne infrared smoke; combat aircraft target; ground infrared countermeasure; infrared homing missile; Aerodynamics; Aircraft; Infrared detectors; Interference; Jamming; Missiles; Optimal control; Tracking; Velocity control; Weapons; airborne infrared smoke; optimal control rule; optimal method; right elusion;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Simulation and Scientific Computing, 2008. ICSC 2008. Asia Simulation Conference - 7th International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-1786-5
Electronic_ISBN :
978-1-4244-1787-2
Type :
conf
DOI :
10.1109/ASC-ICSC.2008.4675428
Filename :
4675428
Link To Document :
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