公开(公告)号：KR100808026B1

公开(公告)日：2008-02-28

申请号：KR1020060123344

申请日：2006-12-06

Applicant: 국방과학연구소

Inventor： 김흥범 ,  이용재 ,  민준기 ,  채성우 ,  백정부

IPC: F41A33/00 ,  F41G7/00

Abstract: A simulator apparatus for flight test system and a simulation method by the same are provided to improve stability for controlling or measuring the test by simulating a flying test measuring system required for the flying test. A simulator apparatus for flight test system comprises a simulator(100), a system interface, a stimulator(110), and a control computer. The simulator simulates a flying test measuring system required for the flying test. The system interface transforms and switches a signal for the simulator and the interface. The simulator transmits the information simulated from the simulator to the system interface. The control computer displays the file transmitted to the system interface. The simulator transmits the signal to the stimulator through an Ethernet. The flying test measuring system consists of a radar measurement for measuring the data for the line of fire to confirm the capacity of weapon system, and a remote measurement for getting the measurement data for the inside operation condition of a guided missile.

Abstract translation: 提供了一种用于飞行测试系统的模拟器装置及其仿真方法，以通过模拟飞行测试所需的飞行测试测量系统来提高用于控制或测量测试的稳定性。 用于飞行测试系统的模拟器装置包括模拟器（100），系统接口，刺激器（110）和控制计算机。 模拟器模拟飞行测试所需的飞行测试测量系统。 系统接口转换并切换模拟器和接口的信号。 模拟器将从模拟器模拟的信息传输到系统接口。 控制计算机显示发送到系统界面的文件。 模拟器通过以太网将信号传输到刺激器。 飞行测试测量系统包括测量火线数据的雷达测量，以确定武器系统的容量，以及获取导弹内部操作状况的测量数据的远程测量。