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DIGITAL SIMULATOR airborne radar systems

机译:数字模拟器机载雷达系统

摘要

The proposed utility model relates to the field of radar, in particular, to devices for monitoring performance of radar systems. Digital simulator airborne radar systems comprises a dummy noise signal simulator response signal antenna attenuators device simulator probe signal simulator leading away signals, the simulator impact signal simulator multiple signal switching device, a radar control system (RCS), the interface device, the apparatus registration, the computer control signals RCS, the simulator display system signals, computer signals executive objects navigation calculator signaling, control and switching unit and a control unit. the bus control unit coupled to the first input of the monitoring and switching unit, a first output connected to the input of the calculator RCS control signals, and the output of the calculator RCS control signals coupled to the first input of the RCS, the second output of the control and switching unit is connected to the input of the simulator display system signals output which is connected to the second input RCS, the third output control and switching unit is connected to the input signal calculator executive objects whose output is connected to the third input RCS. The fourth control output unit and switching coupled to an input navigation signal calculator, whose output is connected to a fourth input of RCS, the fifth control output and the switching unit is connected to the input bus of the switching device, a first output connected to the input signal simulator repeated. Multiple signal simulation output is connected to the first input of the attenuator device, the second output of the switching device connected to the input of the response signal to the simulator, the simulator output response signal is connected to the second input attenuators device. The third output of the switching device connected to the input of the impact simulator signal, the output signal of the impact simulator coupled to the third input of the attenuator device, the fourth output of the switching device connected to the input signal simulator leading away. Leading away simulation output signal is connected to a fourth input of the attenuator device, the fifth output of the switching device connected to an input of the noise simulator; signal. Yield noise signal simulator is coupled to a fifth input attenuators device sixth output of the switching device connected to the input signal of the simulator probe, the probe signal simulation output is connected to the sixth input attenuators device attenuators output device coupled to the antenna. Yield RCS connected to the input coupler, output coupler connected to the input register unit and the output register unit is connected to the second input and a switching control unit. To achieve the possibility of providing the control and adjustment of radar control systems, simulating the operation of the systems of avionics, not only one object, but also the interaction between multiple objects in a group for a single tactical plan introduced simulator control commands, setpoint initial parameters of the target, timing device, target distribution device, the device indication device allocation parameters simulated targets. The second control unit output is connected to the input of the simulator control commands, the first output of which is connected to the initial parameter setting unit purpose, whose output is connected to the first input of the conversion device parameters of simulated targets. The second output of the simulator control commands from a device connected to the time synchronization, the output of which is connected to the second input of the conversion device parameters of the simulated target, the first output of which is connected to the third input of the display device. The second output of simulated targets parameter conversion device is connected to a fifth input of RCS, a second output connected to the input RCS target distribution device, the output target setting device connected to the second input of the indicating device. The second output of the calculator navigation signals connected to the first input of the display device.
机译:本实用新型涉及雷达领域,尤其涉及一种监控雷达系统性能的装置。数字模拟器机载雷达系统包括虚拟噪声信号模拟器响应信号天线衰减器模拟器模拟器探头信号模拟器引出信号,模拟器冲击信号模拟器多信号切换设备,雷达控制系统(RCS),接口设备,设备注册,计算机控制信号RCS,模拟器显示系统信号,计算机对象执行对象,导航计算器信号,控制和切换单元以及控制单元。总线控制单元耦合到监视和切换单元的第一输入,第一输出耦合到计算器RCS控制信号的输入,并且计算器RCS控制信号的输出耦合到RCS的第一输入,第二控制和切换单元的输出连接到模拟器显示系统的信号输入,该信号连接到第二输入RCS,第三输出控制和切换单元连接到输入信号计算器执行对象,其输出连接到第三输入RCS。第四控制输出单元和开关耦合到输入导航信号计算器,其输出连接到RCS的第四输入,第五控制输出,并且开关单元连接到开关装置的输入总线,第一输出连接到输入信号模拟器重复进行。多信号模拟输出连接到衰减器设备的第一输入,开关设备的第二输出连接到模拟器的响应信号的输入,模拟器输出响应信号连接到第二输入衰减器。开关设备的第三输出连接到冲击模拟器信号的输入,冲击模拟器的输出信号耦合到衰减器设备的第三输入,开关设备的第四输出连接到输入信号模拟器的前端。引出模拟输出信号连接到衰减器装置的第四输入端,开关装置的第五输出端连接到噪声模拟器的输入端;信号。良率噪声信号模拟器耦合到第五输入衰减器装置的第六输出,该开关装置的第六输出连接到模拟器探针的输入信号,探针信号模拟输出连接到第六输入衰减器装置的衰减器输出装置,该衰减器输出装置耦合到天线。良率RCS连接到输入耦合器,输出耦合器连接到输入寄存器单元和输出寄存器单元连接到第二输入和开关控制单元。为了实现提供对雷达控制系统进行控制和调节,模拟航空电子系统的操作的可能性,不仅要针对单个战术计划模拟一个对象,还要模拟一组对象中多个对象之间的交互作用,并引入模拟器控制命令,设定值目标的初始参数,计时设备,目标分配设备,设备指示设备,模拟目标分配参数。第二控制单元输出连接到仿真器控制命令的输入,仿真器控制命令的第一输出连接到初始参数设置单元用途,其初始输出连接到模拟目标的转换设备参数的第一输入。来自连接到时间同步的设备的模拟器控制命令的第二输出,该设备的输出连接到模拟目标的转换设备参数的第二输入,该设备的第一输出连接到时间同步的第三输入显示设备。模拟目标参数转换设备的第二输出连接到RCS的第五输入,第二输出连接到输入RCS目标分配设备,输出目标设置设备连接到指示设备的第二输入。计算器导航信号的第二输出连接到显示设备的第一输入。

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