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公开(公告)号：KR1020130076436A
公开(公告)日：2013-07-08
申请号：KR1020110145027
申请日：2011-12-28
Applicant: 국방과학연구소
Abstract: PURPOSE: A communication method of a communication device is provided to efficiently transmit data by using a limited wireless sensor network resource. CONSTITUTION: First variations of data values in a first transmission section are measured according to unit time (S102). An average of the first variations is calculated (S104). A filter value is calculated based on the average value (S110). Each data is filtered in a second transmission section by using the filter value to be transmitted (S200). If the average value is bigger than a first reference value, a dynamic mode is executed in the second transmission section. If the average value is smaller than or same as the first reference value, a static mode is executed in the second transmission section. [Reference numerals] (AA) Start; (BB) End; (S102) Measuring data variations ( first variation )in first transmission section according to unit time; (S104) Calculating average value of the first variations; (S112) First standard value DTR maximum value; (S128) Filter value (DTR-filter)=DTR maximum value; (S200) Filtering data by using filter value (DTR-filter) in second transmission period
Abstract translation: 目的：提供通信设备的通信方法，通过使用有限的无线传感器网络资源来有效地发送数据。 构成：根据单位时间测量第一发送部中的数据值的第一变化（S102）。 计算第一变化的平均值（S104）。 基于平均值计算滤波器值（S110）。 通过使用要发送的滤波器值，在第二发送部分中对每个数据进行滤波（S200）。 如果平均值大于第一参考值，则在第二传输部分中执行动态模式。 如果平均值小于或等于第一参考值，则在第二传输部分中执行静态模式。 （附图标记）（AA）开始; （BB）结束; （S102）根据单位时间测量第一发送部中的数据变化（第一变形） （S104）计算第一变化的平均值; （S112）第一标准值<平均值; （S114）计算低于平均值的滤波器值（DTR_filter）; （S116）计算高于平均值的滤波器值（DTR_filter）; （S122）滤波器值（DTR滤波器）
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公开(公告)号：KR1020130019561A
公开(公告)日：2013-02-27
申请号：KR1020110081577
申请日：2011-08-17
Applicant: 국방과학연구소
Abstract: PURPOSE: A launch control system for a flight test is provided to process control information into various kinds of communication protocols and messages, thereby improving a control function for a guided weapon flight test, and processing various kinds of control signals. CONSTITUTION: A launch control system for a flight test includes a launch control signal processor(130), a system controller(110), a remote controller(160), a control signal distributor(150), a status indicator(140), and a shoot control system(120). The launch control signal processor implements launch control signal transmission/reception, signal treatment, and communication protocol conversion for a target flight vehicle. The system controller manages the entire launch control system including the launch control signal processor, and controls linked equipment. The remote controller interfaces with the shoot control system of a remote location. The control signal distributor interfaces with communication signals between the launch control signal processor and the remote controller. The status indicator indicates launch control information from the control signal distributor, and generates event information, and then transmits the event information to the launch control signal processor. The shoot control system linked with the launch control system for the flight test controls launching procedures for a guided missile through an interface with the launch control signal processor and the control signal distributor. [Reference numerals] (110) System controller; (120) Shoot control system; (130) Launch control signal processor; (140) Status indicator; (150) Control signal distributor; (160) Remote controller; (170) Flight test control computer; (180) Visual countdown device
Abstract translation: 目的：提供用于飞行测试的发射控制系统，以将控制信息处理成各种通信协议和消息，从而提高了导弹武器飞行试验的控制功能，并处理各种控制信号。 构成：用于飞行测试的发射控制系统包括发射控制信号处理器（130），系统控制器（110），遥控器（160），控制信号分配器（150），状态指示器（140）和 射击控制系统（120）。 发射控制信号处理器为目标飞行器实施发射控制信号的发射/接收，信号处理和通信协议转换。 系统控制器管理包括发射控制信号处理器在内的整个发射控制系统，并控制链接的设备。 遥控器与远程位置的拍摄控制系统相连。 控制信号分配器与发射控制信号处理器和遥控器之间的通信信号接口。 状态指示器指示来自控制信号分配器的发射控制信息，并产生事件信息，然后将事件信息发送到发射控制信号处理器。 与飞行测试发射控制系统相关的射击控制系统通过与发射控制信号处理器和控制信号分配器的接口来控制导弹的发射程序。 （附图标记）（110）系统控制器; （120）射击控制系统; （130）启动控制信号处理器; （140）状态指标; （150）控制信号分配器; （160）遥控器; （170）飞行试验控制电脑; （180）视觉倒计时装置
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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
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。
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公开(公告)号：KR102213842B1
公开(公告)日：2021-02-08
申请号：KR1020200135866
申请日：2020-10-20
Applicant: 국방과학연구소
IPC: G06F11/273 , G06F11/22 , G06F9/451 , G06F16/22 , G06F11/263
Abstract: 본발명에따른이종시험장비인터페이스장치가제공된다. 상기이종시험장비인터페이스장치는복수의환경시험챔버에연결되는복수의데이터중간장치, 및상기복수의데이터중간장치와연동하는적어도하나의컴퓨터장치를포함한다. 상기복수의데이터중간장치각각은상기복수의환경시험챔버중에서연동하는적어도하나의환경시험챔버로부터수신되는전기신호를 SNMP 프로토콜에기초하여데이터신호로변환하여출력하고, 상기적어도하나의컴퓨터장치로부터수신되는운용제어명령에따라, 상기연동하는적어도하나의환경시험챔버를제어할수 있는제어신호를출력하도록구성된다.
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Patent Agency Ranking
公开(公告)号：KR1020140124886A
公开(公告)日：2014-10-28
申请号：KR1020110092040
申请日：2011-09-09
Applicant: 국방과학연구소
Abstract: 본 발명은 능동형 RFID를 이용한 분산자탄의 궤적 및 분산도 계측 장치 및 방법에 관한 것으로, 유도/로켓 무기체계에서 탄두로 사용되는 분산자탄; 상기 분산자탄에 부착되어 신호를 발생하는 능동형 RFID; 해상에 탄착하는 분산자탄의 탄착 범위내에서, 상기 분산자탄에 탑재된 능동형 RFID로부터 분산자탄의 RFID 신호 및 GPS 신호를 수신하고, 상기 분산자탄의 GPS 신호를 기준으로 RFID 신호를 송출하고, 육상 지역의 계측정보 수신부로 계측 정보를 송출하는 계측 노드; 육상지역에 위치하며, 상기 계측 노드로부터 전송되는 분산자탄의 정보와 GPS 신호, 위성항법보정시스템(DGPS; Differential Global Positioning System)의 보정신호를 수신하여 자료 수신 및 정밀 자료처리 시스템으로 전달하는 육상지역의 계측 정보 수신부; 및 상기 계측노드로부터 전송된 분산자탄의 GPS 수신 정보, GPS 신호, DGPS 보정신호를 기반으로 상기 계측노드의 위치정보를 보정하고, 계측노드 기준의 분산자탄의 위치를 추정하여, 보정된 계측노드의 위치정보를 기반으로 분산 자탄의 정밀위치를 연산한 후, 이 정보를 비행시험통제소로 전송하는 자료 수신 및 정밀 자료처리 시스템을 포함한다. 이에 따라, 분산자탄을 탄두로 사용하는 유도무기/로켓 무기체계의 자탄 분산도 및 자탄 비행궤적을 계측에 사용될 수 있고, 분산 자탄의 위치를 실시간으로 파악하여 안전한 비행시험을 실시하는 효과가 있다.
Abstract translation: 本发明涉及使用有源RFID测量群集炸弹的踪迹和色散的装置和方法。 使用有源RFID测量集束炸弹的痕迹和色散的装置包括在导向/火箭武器系统中用作弹头的集束炸弹; 连接到集群炸弹的有源RFID产生信号; 测量节点，从安装在所述集群炸弹中的有源RFID接收所述群集轰炸机的RFID信号和GPS信号，基于所述群集炸弹的GPS信号发射RFID信号，并将测量信息发送到测量信息接收单元 在海上的集束炸弹的发现范围内的一个土地面积; 接收位于陆地区域的陆地区域的测量信息接收单元，接收从测量节点发送的群集炸弹和GPS信号的信息和来自差分全球定位系统（DGPS）的校正信号，并且传送接收的信息 集群炸弹，GPS信号和校正信号发送到数据接收和精密处理系统; 以及数据接收和精密处理系统基于从测量节点发送的聚类炸弹的GPS接收信息，GPS信号和DGPS校正信号来校正测量节点的位置信息，估计该测量节点的位置 相对于测量节点的集束炸弹，基于测量节点的校正位置信息计算集群炸弹的精确位置，并将相应的信息发送到测试飞行调节站。 因此，可以使用使用集束炸弹作为弹头的导弹武器/火箭武器系统的炸弹分散和飞行轨迹进行测量，并且可以通过实时识别集束炸弹的位置来执行安全飞行试验。
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公开(公告)号：KR101318237B1
公开(公告)日：2013-10-15
申请号：KR1020110081577
申请日：2011-08-17
Applicant: 국방과학연구소
Abstract: 시험 대상 비행체의 발사통제 신호의 송·수신 및 신호 처리와 통신 프로토콜 변환을 담당하는 발사통제 신호처리기; 발사통제 신호처리기를 포함한 발사통제 시스템 전체를 관리하고 연동장비를 제어하는 시스템 제어기; 원격지의 사격통제 시스템과의 인터페이스를 수행하는 원격 제어기; 발사통제 신호처리기 및 원격 제어기 사이의 통신 신호를 인터페이스하는 통제신호 분배장치; 발사통제 분배장치에 의한 발사통제 정보를 표시하고 이벤트 정보를 생성하여 발사통제 신호처리기에 송신하는 상태표시기를 포함하여 이루어지는 것을 특징으로 하는 비행시험 발사통제 시스템.
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公开(公告)号：KR1020130027911A
公开(公告)日：2013-03-18
申请号：KR1020110091437
申请日：2011-09-08
Applicant: 국방과학연구소
Abstract: PURPOSE: A fire control interlocking signal simulator and a method thereof are provided to simulate FCC/MCC control signals between a guided weapon fire control system and a flight test fire control system, thereby inspecting a connection of the flight test fire control system and a flight test control system and the performance of equipment before an actual flight test. CONSTITUTION: A fire control interlocking signal simulator comprises a fire control system interlocking unit(210), FCC(Fire Control Center)/MCC(Mission Control Center), a fire control signal simulating unit(270), a FCC/MCC control signal processing unit(220), a control signal displaying unit(240), and a fire control system interlocking unit(230). The fire control system interlocking unit is connected to a fire control system of a guided weapon system, receives FCC control signals, and transmits MCC control signals. The FCC/MCC fire control signal simulating unit simulates control signals generated by a flight test fire control system and the fire control system of the guided weapon system, thereby generating simulation control signals. The FCC/MCC control signal processing unit is connected to the fire control system interlocking unit and the FCC/MCC fire control signal simulating unit, thereby processing the reception and the transmission of the simulation control signals. The fire signal displaying unit is connected to the FCC/MCC control signal processing unit and displays real-time control signals or simulated simulation control signals. The fire control system interlocking unit is connected to a signal processor of the flight test fire control system, receives the MCC control signals, and transmits the FCC control signals. [Reference numerals] (200) Fire control interlocking signal simulator; (201) Shooting control system; (202) Signal processor; (203) FCC control signal; (204) MCC control signal; (220) FCC/MCC control signal processing unit; (230) Fire control system interlocking unit; (240) Control signal displaying unit; (270) FCC/MCC control signal simulating unit; (300) Flight test fire control system; (AA) Induced weapon system shooting control system; (BB) Shooting control system interlocking unit; (CC) Simulation signal; (DD) Real-time signal; (EE) Real-time signal + simulation signal
Abstract translation: 目的：提供消防控制联锁信号模拟器及其方法，以模拟导弹武器消防系统与飞行试验消防系统之间的FCC / MCC控制信号，从而检查飞行试验消防系统与飞行的连接 测试控制系统和设备在实际飞行试验前的性能。 消防控制联锁信号模拟器包括消防控制系统互锁单元（210），FCC（消防控制中心）/ MCC（任务控制中心），消防控制信号模拟单元（270），FCC / MCC控制信号处理 单元（220），控制信号显示单元（240）和消防控制系统互锁单元（230）。 消防控制系统互锁单元连接到导弹武器系统的消防系统，接收FCC控制信号，并发送MCC控制信号。 FCC / MCC消防控制信号模拟单元模拟由飞行试验消防系统和指导武器系统的消防系统产生的控制信号，从而产生模拟控制信号。 FCC / MCC控制信号处理单元连接到消防控制系统联锁单元和FCC / MCC火控信号模拟单元，从而处理模拟控制信号的接收和传输。 火情信号显示单元连接到FCC / MCC控制信号处理单元，并显示实时控制信号或模拟仿真控制信号。 消防控制系统联锁单元连接到飞行测试消防系统的信号处理器，接收MCC控制信号，并发送FCC控制信号。 （附图标记）（200）消防控制联锁信号模拟器; （201）射击控制系统; （202）信号处理器; （203）FCC控制信号; （204）MCC控制信号; （220）FCC / MCC控制信号处理单元; （230）消防系统联锁单元; （240）控制信号显示单元; （270）FCC / MCC控制信号模拟单元; （300）飞行试验消防系统; （AA）诱导武器系统射击控制系统; （BB）射击控制系统联锁单元; （CC）模拟信号; （DD）实时信号; （EE）实时信号+模拟信号
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