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公开(公告)号：KR1020140090478A
公开(公告)日：2014-07-17
申请号：KR1020130002579
申请日：2013-01-09
Applicant: 국방과학연구소
Abstract: The present specification relates to an integrated survivability demonstration apparatus of an aircraft which integrates a radar warning receiver, a laser warning receiver, a missile warning receiver, and a chaff/flare dispenser into an avionic system; and a method thereof. According to the present invention, the integrated survivability demonstration apparatus of the aircraft includes: an electronic warfare computer interlocked with a radar warning receiver, a laser warning receiver, a missile warning receiver, and a chaff/flare dispenser. The integrated survivability demonstration apparatus of the aircraft comprises: a plurality of mission computers receiving threat information, state information and response result information; a plurality of multifunctional demonstrators demonstrating the received treat information, state information and response result information by controlling the mission computers; and a plurality of control demonstrators demonstrating a plurality of components.
Abstract translation: 本说明书涉及将航空电子系统中的雷达警报接收器，激光警报接收器，导弹警告接收器和谷壳/火炬分配器集成的飞行器的综合生存性演示装置; 及其方法。 根据本发明，飞行器的综合生存演示装置包括：与雷达警报接收器，激光警告接收器，导弹警告接收器和谷壳/火炬分配器联锁的电子战计算机。 飞机的综合生存能力演示装置包括：多个任务计算机接收威胁信息，状态信息和响应结果信息; 多个多功能示威者，通过控制任务计算机来演示收到的待处理信息，状态信息和响应结果信息; 以及展示多个部件的多个控制演示器。
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公开(公告)号：KR1020140090476A
公开(公告)日：2014-07-17
申请号：KR1020130002577
申请日：2013-01-09
Applicant: 국방과학연구소
CPC classification number: G09B9/42 , G09B9/44 , G09B9/46 , G09B19/165
Abstract: According to an embodiment of the present invention, an aircraft with a training system includes a plurality of multifunctional displays which display flight-related data to a user; and a control unit which controls devices in the aircraft based on user inputs and outputs data from the devices onto the multifunctional displays. In a first mode, the control unit actually controls the devices in the aircraft. In a second mode, the control unit virtually controls the devices in the aircraft, and the result data according to user inputs is outputted onto the multifunctional displays.
Abstract translation: 根据本发明的实施例，具有训练系统的飞机包括多个多功能显示器，其向用户显示飞行相关数据; 以及控制单元，其基于用户输入来控制飞行器中的设备，并将来自设备的数据输出到多功能显示器上。 在第一模式中，控制单元实际控制飞行器中的装置。 在第二模式中，控制单元虚拟地控制飞行器中的装置，并将根据用户输入的结果数据输出到多功能显示器上。
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公开(公告)号：KR101426289B1
公开(公告)日：2014-08-05
申请号：KR1020130002578
申请日：2013-01-09
Applicant: 국방과학연구소
Abstract: 본 명세서는 항공기 계기 비행에 측면 항법을 적용하는 기동 헬기 측면 항법 운용 장치 및 그 방법에 관한 것이다. 이를 위하여 본 명세서에 따른 기동 헬기 측면 항법 운용 장치는, 제1 및 제2 자동 조종 컴퓨터, 데이터 획득 처리 장치 및, 초단파 전방향 거리탐지기와 연동하는 이중 구조로 형성되는 기동 헬기 측면 항법 운용 장치에 있어서, 상기 기동 헬기 측면 항법 운용 장치는, 주요 비행정보 시현 페이지를 표시하며, 상기 표시 중인 주요 비행정보 시현 페이지에서 선택된 항법 소스의 모드를 확인하는 제1, 제2, 제3 및, 제4 다기능시현기; 상기 기동 헬기 측면 항법 구동을 위한 하나 이상의 파라미터 값을 설정하는 제1 및 제2 통제시현장치; 항로 노브를 설정하는 제1 및 제2 비행조종 패널; 및 상기 선택된 항법 소스 모드가 비행 계획, 초단파 전방향 거리탐지기/계기착륙장치, 홈 모드일 때, 상기 제1 및 제2 비행조종 패널의 항로 노브로 설정된 수동 항로 방향을 근거로 계획된 구간을 설정하고, 롤 명령을 계산하는 제1 및 제2 임무 컴퓨터;를 포함한다.
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公开(公告)号：KR1020140092645A
公开(公告)日：2014-07-24
申请号：KR1020130004957
申请日：2013-01-16
Applicant: 국방과학연구소
IPC: G10L25/03 , G10L25/54 , G10L13/033
CPC classification number: G10L25/09 , G10L13/033 , G10L25/54
Abstract: According to a fighter pilot voice command execution method of the present invention, a voice command (fighter command) of a pilot is automatically divided into the word unit and a silent syllable is hidden with the energy processing of a short section signal and zero crossing rage processing. A voice characteristic parameter is determined from a mel-frequency cepstrum coefficient (MFCC) and a recognizing candidate group by the word is set. The recognizing candidate group by the word is formed of a command of a connection word base with a connection word matching technique based on a verbal tree. Therefore, word matching times are reduced dramatically and a recognizing rate of the command is highly increased. Especially, a word recognizing time is reduced by reducing the similarity measuring times.
Abstract translation: 根据本发明的战斗机导航语音指令执行方法，导频的语音命令（战斗机命令）被自动划分为单词单元，并且通过短路信号和过零点的能量处理隐藏无声音节 处理。 从梅尔频率倒谱系数（MFCC）确定语音特征参数，并且设置通过该单词的识别候选组。 该单词的识别候选组由具有基于语言树的连接词匹配技术的连接词库的命令形成。 因此，字匹配时间显着减少，并且命令的识别率高度增加。 特别地，通过减少相似度测量时间来减少字识别时间。
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Patent Agency Ranking
公开(公告)号：KR101427806B1
公开(公告)日：2014-08-07
申请号：KR1020130004957
申请日：2013-01-16
Applicant: 국방과학연구소
IPC: G10L25/03 , G10L25/54 , G10L13/033
Abstract: 본 발명의 전투기 조종사 음성명령실행방법에서는 발화된 조종사의 음성명령어(전투기 명령어)가 단어단위별로 자동분할되어 단구간신호의 에너지 처리와 영 교차율(Zero Crossing Rate)처리로 묵음이 가려지고, MFCC(Mel-Frequency Cepstrum Coefficent)로부터 음성특성 파라미터(Parameter)가 결정됨으로써 각 단어별 인식 후보군이 설정되며, 설정된 단어별 인식 후보군이 구문트리(Verbal Tree)가 기반된 연결단어 정합기술로 연결단어 기반의 명령어로 이루어짐으로써 단어조합 수량을 크게 줄이고 명령어 인식률이 크게 높아지며, 특히 유사도 측정 횟수를 줄여줌으로써 단어 인식시간이 단축되는 특징을 갖는다.
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公开(公告)号：KR1020140090477A
公开(公告)日：2014-07-17
申请号：KR1020130002578
申请日：2013-01-09
Applicant: 국방과학연구소
CPC classification number: G01C21/20
Abstract: The present specification relates to an apparatus and a method for operating lateral navigation in a utility helicopter in which the lateral navigation is applied to aeronautical instrument flying. The apparatus for operating the lateral navigation in the utility helicopter according to the present specification comprises a first, a second, a third, and a fourth multifunctional display for displaying a main flying information display page and for confirming a mode of a navigation source selected in the displayed main flying information display page; a first and a second control apparatus for setting one or more parameter values for operating the lateral navigation in the utility helicopter; a first and a second flying control panel for setting a course knob; and a first and a second assignment computer for setting a section planned based on a manual course direction set by the course knob of the first and the second flying control panel and for calculating a role command when the selected navigation source mode is a flying plan, very high frequency front direction distance detector/instrument landing apparatus, and a home mode in the apparatus for operating the lateral navigation in the utility helicopter having a dual structure connected to a first and a second automatic control computer, a data processor, and the very high frequency front direction distance detector.
Abstract translation: 本说明书涉及一种用于在实用直升机中操作侧向导航的装置和方法，其中侧向导航应用于航空飞行。 根据本说明书的用于在实用直升机中操作侧向导航的装置包括第一，第二，第三和第四多功能显示器，用于显示主飞行信息显示页面并且用于确认在主飞行信息显示页面中选择的导航源的模式 显示主飞行信息显示页面; 第一和第二控制装置，用于设置用于在实用直升机中操作侧向导航的一个或多个参数值; 第一和第二飞行控制面板，用于设置踏板旋钮; 以及第一和第二分配计算机，用于根据由第一和第二飞行控制面板的航向旋钮设置的手动航向方向来设定计划的部分，并且当所选择的导航源模式是飞行计划时计算角色命令， 超高频前方距离检测器/仪器着陆装置，以及用于操作实用直升机中的侧向导航的装置中的家庭模式，其具有连接到第一和第二自动控制计算机，数据处理器和非常 高频前方距离探测器。
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公开(公告)号：KR101649510B1
公开(公告)日：2016-08-22
申请号：KR1020130002579
申请日：2013-01-09
Applicant: 국방과학연구소
Abstract: 본명세서는레이더경보수신기, 레이저경보수신기, 미사일경보수신기및, 채프/플레어발사기등의각각의시현장치를항공전자장치에통합시키는항공기용통합형생존시현장치및 그방법에관한것이다. 이를위하여본 명세서에따른항공기용통합형생존시현장치는, 레이더경보수신기, 레이저경보수신기, 미사일경보수신기및, 채프/플레어발사기와연동하는생존장비관리컴퓨터를포함하는항공기용통합형생존시현장치에있어서, 상기항공기용통합형생존시현장치는, 상기생존장비관리컴퓨터로부터전달되는위협정보, 상태정보및, 대응결과정보를수신하는복수의임무컴퓨터; 상기복수의임무컴퓨터의제어에의해, 상기수신된위협정보, 상태정보및, 대응결과정보를시현하는복수의다기능시현기; 및복수의구성품을시현하는복수의통제시현장치;를포함한다.
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公开(公告)号：KR1020140090867A
公开(公告)日：2014-07-18
申请号：KR1020130003039
申请日：2013-01-10
Applicant: 국방과학연구소
CPC classification number: B64D43/00 , G01C21/20 , G01C23/005
Abstract: The present specification relates to an apparatus for driving required navigation performance of a mobile helicopter and a method thereof for implementing the required navigation performance by flight phase. The apparatus for driving required navigation performance of a mobile helicopter according to the present specification comprises a plurality of multi-functional demonstration devices for displaying a main flight information demonstration page and checking a selected navigation source mode from the main flight information demonstration page in display; a plurality of demonstration control devices for setting one or more parameter values for driving the required navigation performance of the mobile helicopter; and a plurality of mission computers for demonstrating required navigation flight phases on the flight information demonstration page of the multi-functional demonstration devices when the selected navigation source mode is a flight planning and a home mode, and automatically changing a fly-by waypoint and a fly-over waypoint based on required navigation performance conditions by flight phase corresponding to the selected required performance flight phase menu when one is selected from the required performance flight phase menus included in the demonstrated required navigation performance flight phase.
Abstract translation: 本说明书涉及一种用于驾驶移动直升机所需导航性能的装置及其方法，用于通过飞行阶段来实现所需导航性能。 根据本说明书的移动式直升机驾驶所需的导航性能的装置包括多个多功能演示装置，用于显示主飞行信息演示页面，并从显示的主飞行信息演示页面检查所选择的导航源模式; 多个演示控制装置，用于设定用于驱动移动直升机所需导航性能的一个或多个参数值; 以及多个任务计算机，用于在所选择的导航源模式是飞行计划和归属模式时，在多功能演示装置的飞行信息演示页面上演示所需的导航飞行阶段，并且自动地改变飞行路线点和 根据所需的导航性能条件，飞行阶段对应于所选择的所需性能飞行阶段菜单，当从所需的性能飞行阶段菜单中选择包括在演示的所需导航性能飞行阶段时，飞行航路点。
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