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作 者:董康生[1] 曹林平[1] 韩统[1] 黄汉桥[1] 蔡佳[1]
机构地区:[1]空军工程大学航空航天工程学院,陕西西安710038
出 处:《空军工程大学学报(自然科学版)》2013年第2期42-46,共5页Journal of Air Force Engineering University(Natural Science Edition)
基 金:航空科学基金资助项目(20105196016)
摘 要:针对激光成像引信在空空导弹中的应用要解决引信前倾角和引信探测距离的设计问题,在分析激光成像引信推扫成像原理的基础上,建立了激光引信脚印尺寸模型和引信前倾角与探测距离模型,通过仿真得到了最佳引信前倾角和探测距离的设计指标:最佳引信前倾角为15°~40°,相应最佳引信探测距离为70~24m。Laser imaging fuse has a strong anti-stealth and anti-electromagnetic interference capacity. In the application of laser imaging fuse to air-to-air missile the design problems of fuse front rake and fuse detec- tion range have to be solved. Based on analyzing the principle of the push-broom method laser imaging fuse, the measurement model of laser footprint size and the mathematic model of fuse front rake and fuse detection range are established. The design criterion of fuse front rake and fuse detection range and their relationship to fuse-warhead match by simulation in variety conditions are acquired, which provide a refer- ence in theory to the application of laser imaging fuse in air-to-air missile.
关 键 词:激光成像引信 空空导弹 引信前倾角 探测距离 引战配合
分 类 号:TN95[电子电信—信号与信息处理]
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