TY - GEN
T1 - Research on the configuration of airborne infrared flare dispenser
AU - Hu, Yifan
AU - Song, Bifeng
PY - 2010
Y1 - 2010
N2 - The study aims to evaluate the infrared (IR) flare effectiveness and summarize the configuration principles of airborne IR flare dispenser, with the simulation method, which consists of aircraft model, missile model, and flare system model. Based on this method, the successful decoy probabilities PJ under different engagement situations are calculated, and the effect of two important configuration parameters, installation position and direction, on the effectiveness is analyzed. According to the results and analysis, it is summarized that installation direction contributes greatly to flare effectiveness. If the missile velocity change due to flare dispensing direction is opposite to the change due to aircraft, the dispenser installation direction is more effective to seduce the missile. The influence of installation position is reflected only when the flares are dispensed at a short range. Moreover, flare dispenser should be installed near the IR centroid of aircraft to appear immediately in seeker field of view (FOV) and function as long as possible.
AB - The study aims to evaluate the infrared (IR) flare effectiveness and summarize the configuration principles of airborne IR flare dispenser, with the simulation method, which consists of aircraft model, missile model, and flare system model. Based on this method, the successful decoy probabilities PJ under different engagement situations are calculated, and the effect of two important configuration parameters, installation position and direction, on the effectiveness is analyzed. According to the results and analysis, it is summarized that installation direction contributes greatly to flare effectiveness. If the missile velocity change due to flare dispensing direction is opposite to the change due to aircraft, the dispenser installation direction is more effective to seduce the missile. The influence of installation position is reflected only when the flares are dispensed at a short range. Moreover, flare dispenser should be installed near the IR centroid of aircraft to appear immediately in seeker field of view (FOV) and function as long as possible.
KW - Configuration
KW - Dispenser
KW - Installation direction
KW - Installation position
KW - IR flare
KW - Simulation
UR - http://www.scopus.com/inward/record.url?scp=84914142024&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:84914142024
T3 - Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010
SP - 612
EP - 615
BT - Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010
PB - Northwestern Polytechnical University
T2 - 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010
Y2 - 13 September 2010 through 15 September 2010
ER -