首页> 外国专利> method and device for protection against u043fu0440u043eu0442u0438u0432u043eu0440u0430u0434u0438u043eu043bu043eu043au0430u0446u0438u043eu043du043du044bu0445 missile precision tracking radar station

method and device for protection against u043fu0440u043eu0442u0438u0432u043eu0440u0430u0434u0438u043eu043bu043eu043au0430u0446u0438u043eu043du043du044bu0445 missile precision tracking radar station

机译:防止 u043f u0440 u043e u0442 u0438 u0432 u043e u0440 u0430 u0434 u0438 u043e u043e u043b u043e u043a u0430 u0446 u0446 u0438 u043e u043d u043d u043b u0445导弹精确跟踪雷达站

摘要

for a patent submitted by way of u043fu0440u043eu0442u0438u0432u043eu043bu043eu043au0430u0446u0438u043eu043du043du044bu0445 missiles (ors) radar station accurate tracking, which isfor the protection of aircraft use n diversionary sources (oi), frequency and time parameters which are identical with the corresponding pairs of radiation u0435u0442u0440u0430u043cu0438 radiation radarwith the fact that the radiation radar in air are in u043fu0440u0435u0440u044bu0432u0438u0441u0442u043eu043c mode and radiation oh - in the pauses between u0438u0437u043bu0443u0447u0435u043du0438u044fu043cu0438 radarand during each pause is consistently radiation of at least two oi, and their total radiation time in each cycle of the airing exceeds its u0436u0438u0442u0435u043bu044cu043du043eu0441u0442u044c radiation radar.the n he is worn in the top of convex u043cu043du043eu0433u043eu0443u0433u043eu043bu044cu043du0438u043au0430, one of which is a radar, and within the station areathe limited size of the spatial selection of homing head ors, and the cycle of the radar in the ether choose less continuous time control ors for the management.the device, developed u0437u0430u044fu0432u043bu044fu0435u043cu044bu0439 way contains n diversionary emitters with blocks of the n lines with the exchange control device - take it easy.in turn, the road interchange with the radar control device.each oi contains sequentially the block interchange, the control unit of the transmitter, the transmitter, the output of which power dividers and directional couplers p u043eu0434u043au043bu044eu0447u0435u043d to the antenna.the second gate is designed u043eu0442u0432u0435u0442u0432u0438u0442u0435u043bu044f connected block control outlet connected to a control gate control unit transmitter.autonomous work he is self-contained with a power supply, a post connected to a feeder u0432u0445u043eu0434u0430u043c
机译:通过 u043f u0440 u043e u0442 u0438 u0432 u043e u043b u043b u043e u043a u0430 u0446 u0438 u043e u043d u043d u044d u044b u0445提交的专利跟踪,这是为了保护飞机而使用的n个转向源(oi),频率和时间参数与相应的辐射对对相同,但实际上,空气处于 u043f u0440 u0435 u0440 u044b u0432 u0438 u0441 u0442 u043e u043c模式和辐射哦-在 u0438 u0437 u043b u0443 u0447 u0435 u043d u0438之间的停顿在每个暂停期间,雷达始终辐射至少两个oi,并且在每个播音周期中,它们的总辐射时间超过了其辐射时间。 u0442 u044c辐射雷达。他戴在凸面 u043c u043d u043e u0433 u043e u043e u0443 u0433 u043e u043b u044c u043d u0438 u043a u0430的顶部, ch是一台雷达,并且在站区内有限的归巢头空间选择空间,而雷达在以太周期内选择较少的连续时间进行控制。该装置,研制成功。 u0432 u043b u044f u0435 u043c u044b u0439方式包含n个带有发射控制装置的n行线路的分流发射器-放轻松。反过来,与雷达控制装置进行道路互换。每个oi都包含依次将块交换,发射机的控制单元,发射机,功率分配器和定向耦合器的输出p u043e u0434 u043a u043b u044e u0447 u0435 u043d连接到天线。 u043e u0442 u0432 u0435 u0442 u0432 u0438 u0442 u0435 u043b u044f已连接的块控制插座已连接至控制门控制单元变送器。自主工作他是独立的,有电源,已连接接线柱到进纸器 u0432 u0445 u043e u0434 u0430 u043c

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