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1. 发明授权

KR102088041B1 외부운용환경에 대한 적응형 진행파관증폭기의 출력제어장치 및 방법 有权
公开(公告)号：KR102088041B1
公开(公告)日：2020-03-11
申请号：KR1020190159257
申请日：2019-12-03
申请人： 엘아이지넥스원 주식회사
发明人： 이기욱 , 이왕용
IPC分类号： H03F3/58 , H01J25/49

2. 发明授权

KR101031871B1 신호 대역 선택 장치 및 그 방법 有权
标题翻译：选择信号带的装置和方法
公开(公告)号：KR101031871B1
公开(公告)日：2011-05-02
申请号：KR1020100018034
申请日：2010-02-26
申请人： 엘아이지넥스원 주식회사
发明人： 최혁재 , 이왕용
IPC分类号： G01S7/38 , H03B21/00
摘要： PURPOSE: A device and method for selecting a signal band are provided to simplify a system configuration and reduce calculation time. CONSTITUTION: A detecting unit(110) sorts an input signal according to a frequency band and detects a detection signal. An oscillation signal determining unit(120) selects a specific oscillation signal according to the detected signal. A mixed signal generating unit(130) mixes the input signal with the determined oscillation signal and generates the mixed signal. A band selecting unit(140) selects the band of the output signal by using the mixed signal.
摘要翻译：目的：提供一种用于选择信号频带的设备和方法，以简化系统配置并减少计算时间。构成：检测单元（110）根据频带对输入信号进行排序，并检测检测信号。振荡信号确定单元（120）根据检测到的信号选择特定的振荡信号。混合信号生成单元（130）将输入信号与所确定的振荡信号进行混合，并产生混合信号。频带选择单元（140）通过使用混合信号来选择输出信号的频带。

3. 发明授权

KR102088046B1 디지털 적산에 기반한 고출력증폭기의 적응형 제어장치 및 방법 有权
公开(公告)号：KR102088046B1
公开(公告)日：2020-03-11
申请号：KR1020190159380
申请日：2019-12-03
申请人： 엘아이지넥스원 주식회사
发明人： 이기욱 , 이왕용
IPC分类号： H03F1/02 , H03F1/30 , H03F3/195 , G05B11/40

4. 发明授权

KR101420310B1 미사일 기만기 有权
标题翻译： MISSILE DECOY
公开(公告)号：KR101420310B1
公开(公告)日：2014-07-17
申请号：KR1020140014224
申请日：2014-02-07
申请人： 엘아이지넥스원 주식회사
发明人： 이왕용 , 백대진 , 황성환 , 김성남
IPC分类号： F41H11/02 , F42B12/70
摘要： The present invention provides a missile decoy. The missile decoy includes: a body; a thrust section arranged on the front end of the body, and including a folded first rotor and a motor unit rotating the first rotor; a torque offsetting unit arranged on the rear end of the body, and including a folded second rotor; a decoy device arranged inside the body to receive a frequency signal from enemy′s missile and amplify and transmit the received frequency signal; an inertia measuring unit arranged inside the body; and a control unit configured to control the thrust section and the torque offsetting unit. Therefore, a response time up to the maximum output can be shortened as compared with a body using a jet engine, production properties can be improved, and costs can be reduced by providing the thrust section including rotor blades formed in an upper end of the body and the torque offsetting unit including tail booms formed at the lower end of the body. In addition, a great advantage can be obtained in view of costs, production properties, recycling properties, etc. as compared with a solid-propellent method, and the missile decoy can be made more compact than other bodies.
摘要翻译：本发明提供一种导弹诱饵。导弹诱饵包括：一个身体; 布置在所述主体的前端的推力部，并且包括折叠的第一转子和使所述第一转子旋转的马达单元; 扭矩补偿单元，布置在所述主体的后端，并且包括折叠的第二转子; 设置在身体内的诱饵装置，以接收来自敌方导弹的频率信号，并放大和发送接收到的频率信号; 布置在体内的惯性测量单元; 以及控制单元，被配置为控制推力部和扭矩补偿单元。因此，与使用喷气发动机的机体相比，可以缩短直到最大输出的响应时间，可以提高生产性能，并且可以通过设置包括形成在主体的上端的转子叶片的推力部来降低成本并且扭矩抵消单元包括形成在主体的下端的尾臂。此外，与固体推进法相比，考虑到成本，生产性能，回收性能等方面可以获得很大的优点，导弹诱饵可以比其他物体更紧凑。

5. 发明授权

KR101420307B1 송수신 신호 격리 방식 기반 미사일 기만기 有权
标题翻译：基于发送和接收信号隔离类型的故障诊断
公开(公告)号：KR101420307B1
公开(公告)日：2014-07-17
申请号：KR1020140014258
申请日：2014-02-07
申请人： 엘아이지넥스원 주식회사
发明人： 이왕용 , 백대진
IPC分类号： F41H11/02 , F42B12/70
摘要： A missile decoy based on a transmitting and receiving signal isolated type is disclosed. According to the present invention, the missile decoy based on the transmitting and receiving signal isolated type includes: a body having the inside coated with an electromagnetic wave absorbing coat for isolation of signals between a transmission antenna and a reception antenna; a thrust section arranged on the front end of the body, and including a folded first rotor and a motor unit rotating the first rotor; a torque offsetting unit arranged on the rear end of the body, and including a folded second rotor; a decoy device arranged inside the body to receive a frequency signal from the other missile and amplify and transmit the received frequency signal; an inertia measuring unit arranged inside the body; and a control unit configured to control the thrust section and the torque offsetting unit. The decoy device includes: a reception antenna arranged on an upper end to receive the frequency signal from the other missile; an amplification module configured to amplify a decoy signal; and a rotary transmission antenna arranged on a lower end to transmit the amplified decoy signal in a missile direction.
摘要翻译：公开了一种基于发射和接收信号隔离型的导弹诱饵。根据本发明，基于发送和接收信号隔离型的导弹诱饵包括：内部涂有电磁波吸收涂层的主体，用于隔离发射天线和接收天线之间的信号; 布置在所述主体的前端的推力部，并且包括折叠的第一转子和使所述第一转子旋转的马达单元; 扭矩补偿单元，布置在所述主体的后端，并且包括折叠的第二转子; 设置在身体内的诱饵装置，以从另一导弹接收频率信号，并放大和发送接收的频率信号; 布置在体内的惯性测量单元; 以及控制单元，被配置为控制推力部和扭矩补偿单元。诱饵装置包括：设置在上端的接收天线，用于从另一导弹接收频率信号; 被配置为放大诱饵信号的放大模块; 以及设置在下端的旋转传输天线，以沿导弹方向发射放大的诱饵信号。

6. 发明授权

KR101167160B1 레이더 펄스 신호 검출 장치 有权
标题翻译：用于检测雷达脉冲信号的装置
公开(公告)号：KR101167160B1
公开(公告)日：2012-07-24
申请号：KR1020110047774
申请日：2011-05-20
申请人： 엘아이지넥스원 주식회사
发明人： 곽창민 , 이왕용
IPC分类号： G01S7/285
摘要： PURPOSE: A radar pulse signal detecting device is provided to effectively detect a radar pulse signal under the environment in which continuous waves and noises are mixed. CONSTITUTION: A radar pulse signal detecting device comprises a video detector(110), a comparator(120), a pulse width measuring unit(130), a continuous wave determining unit(140), a frequency based pulse determining unit(150), and a threshold value setup unit(160). The video detector detects an envelope of an input signal and creates a video signal. The comparator compares the video signal with a threshold value and outputs a digital pulse according to the comparison result. The pulse width measuring unit measures pulse width of the digital pulse. The threshold value setup unit changeably establishes the threshold value according to the intensity of the video signal in case the pulse width is higher than a predetermined standard value. The continuous wave determining unit outputs a first control signal in case the pulse width is higher than the predetermined standard value.
摘要翻译：目的：提供雷达脉冲信号检测装置，在连续波和噪声混合的环境下有效地检测雷达脉冲信号。构成：雷达脉冲信号检测装置包括视频检测器（110），比较器（120），脉宽测量单元（130），连续波确定单元（140），基于频率的脉冲确定单元（150）和阈值设定单元（160）。视频检测器检测输入信号的包络并创建视频信号。比较器将视频信号与阈值进行比较，并根据比较结果输出数字脉冲。脉冲宽度测量单元测量数字脉冲的脉冲宽度。在脉冲宽度高于预定标准值的情况下，阈值设定单元根据视频信号的强度可变地建立阈值。连续波确定单元在脉冲宽度高于预定标准值的情况下输出第一控制信号。

7. 发明授权

KR101014771B1 고속 신호 처리 장치 및 방법 有权
标题翻译：装置和处理高速信号的方法
公开(公告)号：KR101014771B1
公开(公告)日：2011-02-14
申请号：KR1020100016588
申请日：2010-02-24
申请人： 엘아이지넥스원 주식회사
发明人： 신규식 , 이왕용
IPC分类号： H03M1/12
CPC分类号： H04L27/0002 , G11C27/02 , H03M1/12 , H03M1/1245 , H03M2201/196
摘要： PURPOSE: An apparatus and a method for processing a high speed signal are provided to efficiency process high speed signal by changing processing speed according to the outside and inside of a programmable logic device. CONSTITUTION: A high speed signal processing apparatus generates sampling data by sampling an analog signal(710) The high speed signal processing apparatus processes sampling data in order to make the transfer rate of sampling data less than a first-transfer rate. The high speed signal processing apparatus processes sampling data in order to enhance the transfer rate of sampling data over a second transfer rate(720) The high speed signal processing apparatus changes the outputted sampling data into an analog signal(730).
摘要翻译：目的：提供一种用于处理高速信号的装置和方法，以通过根据可编程逻辑器件的外部和内部改变处理速度来高效处理高速信号。构成：高速信号处理装置通过对模拟信号进行采样来生成采样数据（710）高速信号处理装置处理采样数据，以使采样数据的传送速率小于第一传送速率。高速信号处理装置处理采样数据，以提高采样数据在第二传送速率上的传送速率（720）。高速信号处理装置将输出的采样数据改变为模拟信号（730）。

8. 发明授权

KR102241425B1 모의신호 송수신시스템 및 제어방법 有权
公开(公告)号：KR102241425B1
公开(公告)日：2021-04-16
申请号：KR1020190141510
申请日：2019-11-07
申请人： 엘아이지넥스원 주식회사
发明人： 김동문 , 이성의 , 이왕용
IPC分类号： G01S7/40
摘要： 본발명은모의신호송수신시스템에관한것으로, 더욱상세하게는모의신호송신출력신호에대한검증과보정을수행하여, 자체품질검증을수행할수 있는모의신호송수신시스템및 제어방법에관한것이다. 본발명의모의신호송수신시스템은시뮬레이션프로그램에기초하여전자전장비의성능을검증하기위한다양한위협에대한모의신호를생성하는신호생성부; 신호생성부에서생성된모의신호를방사하는신호방사부; 신호방사부에서방사된모의신호를전자전장비에대한수신설정값에근거하여수신하는신호수신부; 및신호방사부의최종송신출력과, 신호수신부의수신신호를기준신호와각각비교하고, 각파라미터에따라서기설정된허용오차범위내에포함되는지를판단하여, 모의신호에대한최종송신출력과수신신호를검증하는신호검증부를포함한다.

9. 发明授权

KR101420299B1 관성 모멘트를 이용하여 자세를 안정화하는 미사일 기만기 및 이의 운용 방법 有权
标题翻译：使用惯性和其操作方法进行稳定的错误
公开(公告)号：KR101420299B1
公开(公告)日：2014-07-17
申请号：KR1020140014213
申请日：2014-02-07
申请人： 엘아이지넥스원 주식회사
发明人： 이왕용 , 백대진
IPC分类号： F41H11/02 , F42B12/70
摘要： The present invention provides a missile decoy for stabilizing the position using moment of inertia and a method for operating the same. The missile decoy of the present invention includes: a cylindrical body; a thrust section arranged on the rear end of the body to provide thrust with the body; an inertia moment generating unit arranged on the front end of the body to generate moment of inertia for stabilizing the position of the body; a decoy unit arranged inside the body to receive a frequency signal from the other missile and amplify and transmit the received frequency signal; an inertia measuring unit arranged inside the body, and provided with a plurality of sensors for acquiring position information for position controlled flight; and a control unit configured to control the thrust section and the decoy unit by receiving the position information.
摘要翻译：本发明提供一种使用惯性矩稳定位置的导弹诱饵及其操作方法。本发明的导弹诱饵包括：圆柱体; 推力部分布置在主体的后端以与身体提供推力; 惯性力矩产生单元，布置在身体的前端以产生用于稳定身体位置的惯性矩; 设置在身体内的诱饵单元，以从另一导弹接收频率信号，并放大并发送接收到的频率信号; 惯性测量单元，其布置在所述主体内部，并且设置有用于获取位置控制飞行的位置信息的多个传感器; 以及控制单元，被配置为通过接收位置信息来控制推力部和诱饵单元。

10. 发明授权

KR102022284B1 전자표적 생성장치 및 그 동작방법 有权
公开(公告)号：KR102022284B1
公开(公告)日：2019-09-18
申请号：KR1020180157162
申请日：2018-12-07
申请人： 엘아이지넥스원 주식회사
发明人： 이성의 , 박선영 , 김호준 , 이왕용
IPC分类号： G01S7/02 , G09B9/54

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