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Effect of pre-emptive flares on Man-Portable Air-Defence (MANPAD) systems with a track angle bias counter-countermeasure (CCM)

机译:先发火光对带有航迹角偏置对策(CCM)的便携式防空(MANPAD)系统的影响

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Man-Portable Air-Defence (MANPAD) systems can employ a range of counter-countermeasures (CCM) to reject expendable IR decoys. Three hypothetical MANPAD models are based on reticle types and CCM features that may be found in 1~(st) and 2~(nd) generation MANPADs. These are used in simulations to estimate the probability of escaping hit (PEH) when no IR decoys are used, when IR decoys are deployed reactively and when decoys are deployed preemptively. These cases are simulated for seekers with no CCM and with a track angle bias CCM.rnThe results confirm that the rise rate CCM significantly reduces the PEH when IR decoys are used reactively. The use of pre-emptive flares timed to deploy at or about the time when the seeker is uncaged increases the PEH significantly. A more detailed investigation of the effects of aircraft aspect angle and flare timing on miss distance was carried out to examine the effects of the CCM compared with no CCM. With the aircraft at an altitude of 1000m and a range of 2km there is a critical period in which a flare needs to be released in order to achieve a significant miss distance when the CCM is in use. The conical scan seeker used with the track angle bias CCM was the most effective combination requiring the shortest time during which the flare had to be deployed. Further simulations at longer ranges and different aircraft azimuth angles showed that there is a time window that is range dependant during which pre-emptive decoys are fully effective independently of the aircraft azimuth or threat direction.
机译:便携式防空(MANPAD)系统可以采用多种反制(CCM)来拒绝消耗性的红外诱饵。三种假设的MANPAD模型基于第1代和第2代MANPAD中的标线片类型和CCM特征。在不使用IR诱饵,IR诱饵进行反作用部署以及诱饵先发部署时,这些变量用于仿真中以估计逃逸命中率(PEH)的可能性。这些情况是针对没有CCM且具有航迹角偏差CCM的搜寻器进行仿真的。结果证实,当反应堆使用IR诱饵时,上升速率CCM会显着降低PEH。当导引头未笼罩时或大约在未导引头时,使用预先部署的抢先耀斑会大大增加PEH。进行了飞机长相角和闪光时间对未命中距离的影响的更详细研究,以检查CCM与没有CCM相比的影响。当飞机在1000m的高度和2km的范围内时,有一个关键时期,在这个关键时期,在使用CCM时需要释放眩光以实现较大的失误距离。与航迹角偏置CCM一起使用的锥形扫描寻道器是最有效的组合,需要在最短的时间内展开火炬。在更长的航程和不同的飞机方位角上的进一步仿真显示,存在一个取决于范围的时间窗,在此期间,先发诱饵完全独立于飞机方位角或威胁方向而有效。

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