-
公开(公告)号：KR101779898B1
公开(公告)日：2017-09-19
申请号：KR1020150134111
申请日：2015-09-22
Applicant: 국방과학연구소
Abstract: 본발명은대용량임무자료를고속으로장입처리할수 있는유도무기시스템및 그의임무자료장입방법에관한것으로, 표적및 지형의대용량임무자료를전송하는발사통제장비; 및발사통제장비에서전송된대용량임무자료에대한인터럽트처리루틴및 임무자료메시지처리태스크를수행하여임무자료메시지를처리하는유도조정장치를포함하여구성되며, 상기발사통제장비는임무자료에포함된메시지타입에따라상이한장입모드에서상이한전송방식으로임무자료를전송하는것을특징으로한다.
Abstract translation: 本发明涉及一种能够高速地对高速任务数据进行收费的感应武器系统以及对任务数据进行收费的方法，并且包括用于传输目标和地形的大容量任务数据的发射控制装置; 以及感应调整装置，通过对从发射控制装置发送的大容量任务数据执行中断处理例程和任务数据消息处理任务来处理任务数据消息，其中发射控制装置包括消息 并根据不同的充电模式根据不同的充电模式在不同充电模式下传输任务数据。
-
公开(公告)号：KR101312315B1
公开(公告)日：2013-09-27
申请号：KR1020110093093
申请日：2011-09-15
Applicant: 국방과학연구소
Abstract: 본 명세서는 비행 모의 환경에서 탑재 장비들과 다수의 장치로 이루어진 유도 무기 시스템의 전기, 기계적 인터페이스 및 그 성능을 확인할 수 있는 비행 모의 장치 및 그 방법에 관한 것이다. 본 명세서의 실시예에 따른 비행 모의 장치는, 유도탄의 모의 관성 항법 데이터를 산출하기 위한 유도탄 정보를 발생하는 유도 무기 시스템과; 상기 통신 버스를 통해 상기 유도 조종 장치와 연결되고, 상기 유도탄이 발사될 때 발생하는 발사 신호가 수신되면 유도탄 정보를 근거로 모의 관성 항법 데이터를 산출하는 지상 장비와; 상기 통신 버스를 통해 상기 유도 조종 장치와 연결되고, 상기 유도탄의 발사를 제어하는 발사 제어 장비를 포함할 수 있다.
-
Patent Agency Ranking
公开(公告)号：KR101257688B1
公开(公告)日：2013-04-24
申请号：KR1020110116623
申请日：2011-11-09
Applicant: 국방과학연구소
Abstract: PURPOSE: A method and an apparatus for computing the thrust diagram of a rocket are provided to predict the thrust characteristic of the rocket in real time. CONSTITUTION: A method for computing the thrust diagram of a rocket is as follows: a step for preprocessing to analyze the characteristic of nominal thrust(S110); a step for storing data in the preprocessing step(S120); a step for measuring thrust acceleration in a linearization section(S130); a step for estimating the combustion time of the rocket by using the combustion time of the nominal thrust, the coefficient of a linear approximate function, and the thrust acceleration(S140); and a step for computing the thrust diagram of the rocket based on a nominal thrust diagram and the estimated combustion time of the rocket(S150). [Reference numerals] (AA) Start; (BB) End; (S110) Performing a pre-process for analyzing the characteristics of nominal thrust; (S120) Storing data obtained through the pre-process; (S130) Measuring an acceleration in a linearization section of nominal thrust diagram; (S140) Estimating a rocket combustion time; (S150) Computing a rocket thrust diagram;
Abstract translation: 目的：提供一种用于计算火箭推力图的方法和装置，用于实时预测火箭的推力特性。 构成：计算火箭推力图的方法如下：预处理分析名义推力特性的步骤（S110）; 用于在预处理步骤中存储数据的步骤（S120）; 用于测量线性化部分中的推力加速度的步骤（S130）; 通过使用公称推力的燃烧时间，线性近似函数的系数和推力加速度来估计火箭的燃烧时间的步骤（S140）; 以及基于标称推力图和火箭的估计燃烧时间来计算火箭的推力图的步骤（S150）。 （附图标记）（AA）开始; （BB）结束; （S110）进行名义推力特性分析的预处理; （S120）存储通过预处理获得的数据; （S130）测量标称推力图的线性化部分的加速度; （S140）估计火箭燃烧时间; （S150）计算火箭推力图;
-
公开(公告)号：KR1020130029674A
公开(公告)日：2013-03-25
申请号：KR1020110093093
申请日：2011-09-15
Applicant: 국방과학연구소
Abstract: PURPOSE: A flight simulator and a method thereof are provided to confirm electricity of a guided weapon system comprising a plurality of devices and mounting devices, mechanical interface, and performance in a simulated flight condition. CONSTITUTION: A flight simulator comprises a guided weapon system(100), a ground device(200), and a firing control device (300). The guided weapon system comprises a plurality of mounting devices(120-122) and a guide control device connected through the mounting devices and a communication bus and generates guided missile information for calculating a data of a simulated inertia navigation system of a guided missile. The ground device is connected to the guide control device through the communication bus and calculates the data of the simulated inertia navigation system based on guided missile information when a firing signal of the guided missile is received. The firing control device is connected to the guide control device through the communication bus and controls the firing of the guide missile. [Reference numerals] (110) Guided operation device; (120) Mounted device A; (121) Mounted device B; (122) Mounted device C; (200) Ground device; (300) Firing control device; (AA,BB) Communication bus
Abstract translation: 目的：提供一种飞行模拟器及其方法，用于在模拟飞行状态下确认包括多个装置和安装装置，机械界面和性能的导向武器系统的电力。 构成：飞行模拟器包括导向武器系统（100），地面装置（200）和击发控制装置（300）。 导弹武器系统包括多个安装装置（120-122）和通过安装装置连接的引导控制装置和通信总线，并且产生用于计算导弹的模拟惯性导航系统的数据的导弹信息。 地面装置通过通信总线连接到引导控制装置，并且当接收到导弹的发射信号时，基于导弹信息计算模拟惯性导航系统的数据。 射击控制装置通过通信总线连接到引导控制装置，并控制导弹的射击。 （附图标记）（110）引导操作装置; （120）安装的装置A; （121）安装装置B; （122）安装装置C; （200）接地装置; （300）发射控制装置; （AA，BB）通讯总线
-
公开(公告)号：KR101244699B1
公开(公告)日：2013-03-19
申请号：KR1020110092688
申请日：2011-09-14
Applicant: 국방과학연구소
Abstract: PURPOSE: A Data transmission device of a flight system and a method thereof are provided to easily transmit and receive the software of the mounted equipment without disassembling or reassembling a guided weapon system or a similar system when a developer, an acquirer, or an operator requires modification. CONSTITUTION: Ground equipment(200) generates a start command notifying data transmission start and transmits the start command through a first communication message. The ground equipment generates a second communication message including data. A guided control device(110) forms a communication network with specific mounted equipment(120-122) based on the first communication message. The guided control device transmits the data to the specific mounted equipment. The guided control device receives copy data for the data from the specific mounted equipment. The guided control device transmits the copy data to the ground equipment through a third communication message. [Reference numerals] (110) Guided control device; (120) Onboard equipment A; (121) Onboard equipment B; (122) Onboard equipment C; (200) Ground equipment; (300) Launch control equipment; (AA,BB) Communication bus
Abstract translation: 目的：提供一种飞行系统的数据传输装置及其方法，以便在开发人员，获取方或操作员要求的情况下轻松地传送和接收所安装设备的软件，而无需拆卸或重新组装导向武器系统或类似系统 修改。 构成：地面设备（200）产生通知数据传输开始的启动命令，并通过第一通信消息发送开始命令。 地面设备产生包括数据的第二通信消息。 导向控制装置（110）基于第一通信消息与特定的安装设备（120-122）形成通信网络。 引导控制装置将数据发送到特定的安装设备。 引导控制装置接收来自特定安装设备的数据的复制数据。 引导控制装置通过第三通信消息将复制数据发送到地面设备。 （附图标记）（110）引导控制装置; （120）机载设备A; （121）机载设备B; （122）车载设备C; （200）地面设备; （300）发射控制设备; （AA，BB）通信总线
-
公开(公告)号：KR1020170035249A
公开(公告)日：2017-03-30
申请号：KR1020150134111
申请日：2015-09-22
Applicant: 국방과학연구소
CPC classification number: F42B15/01 , F41G9/00 , G06F9/4812
Abstract: 본발명은대용량임무자료를고속으로장입처리할수 있는유도무기시스템및 그의임무자료장입방법에관한것으로, 표적및 지형의대용량임무자료를전송하는발사통제장비; 및발사통제장비에서전송된대용량임무자료에대한인터럽트처리루틴및 임무자료메시지처리태스크를수행하여임무자료메시지를처리하는유도조정장치를포함하여구성되며, 상기발사통제장비는임무자료에포함된메시지타입에따라상이한장입모드에서상이한전송방식으로임무자료를전송하는것을특징으로한다.
-
公开(公告)号：KR100780807B1
公开(公告)日：2007-11-30
申请号：KR1020060087403
申请日：2006-09-11
Applicant: 국방과학연구소
Abstract: A digital onboard using a squib device test circuit is provided to increase survival of a guided missile and operation of a system for the guided missile by checking errors of a squib driving circuit and a wire from a distance. A digital onboard using a squib device test circuit comprises a communication device, a micro processor, and the squib device test circuit. The communication device enables a guided missile to communicate with a guided missile launching control device at a long distance. The micro processor controls the communication device. The squib device test circuit tests a squib device. The squib device sends and receives a test current to the squib device test device. The squib device test device includes a squib device direct connection circuit(1), a test current generating circuit(2), and a squib device equivalent resistance measuring circuit(3). The squib device direct connection circuit groups a plurality of squib devices as one. The test current generating circuit feeds test current of 1mA to the squib device direct connection circuit. The squib device equivalent resistance measuring circuit receives test current from the squib device direct connection circuit to measure voltage applied to equivalent resistance of the squib device. A self-diagnosis circuit is installed in the test current generating circuit.
Abstract translation: 提供使用爆管装置测试电路的数字板载，以通过从远距离检查爆管驱动电路和电线的误差来增加导弹的生存和用于导弹的系统的操作。 使用爆管装置测试电路的数字板载包括通信装置，微处理器和爆管装置测试电路。 通信装置使得导弹能够与长距离的导弹发射控制装置进行通信。 微处理器控制通信设备。 爆管装置测试电路测试爆管装置。 爆管装置向爆管装置测试装置发送并接收测试电流。 爆管装置测试装置包括爆管装置直接连接电路（1），测试电流产生电路（2）和爆管装置等效电阻测量电路（3）。 爆管装置直接连接电路将多个爆管装置组合为一个。 测试电流发生电路向点火装置直接连接电路馈送1mA的测试电流。 爆管装置等效电阻测量电路从点火装置直接连接电路接收测试电流，以测量施加到点火装置的等效电阻的电压。 自检电路安装在测试电流产生电路中。
-
-
-
-
-
-
Search Results
7
records
(took 0.021 seconds)
