• Electronics and Telecommunications Trends
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• v.38 no.2
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• pp.12-25
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• 2023

Positioning, navigation, and timing information has become a key element in the national core infrastructure and for emerging technologies, such as autonomous driving, lunar exploration, financial systems, and drones. Therefore, the provision of that information by navigation satellite systems is becoming increasingly important. Existing systems such as GPS (Global Positioning System), GLONASS (GLObal NAvigation Satellite System), and BDS (BeiDou Navigation Satellite System) also provide augmentation, safety-of-life, search & rescue and short message communication and authentication services to increase their competitiveness. Those services and the signals generated for their provision have their own purpose and requirements. This article presents an overview of existing or planned satellite navigation satellite system services and signals, aiming to help understand their current status.

• Journal of Satellite, Information and Communications
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• v.12 no.3
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• pp.54-62
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• 2017

China has invested for military satellite technology development to construct the space-based surveillance system from existing land-based and aerostat surveillance system since 1960s to react rapidly for deployment of marine force of United States and surrounding nations in west Pacific, south China sea and Indian ocean. China has also launched about 40 the Yaogan military intelligence satellites series for EO, SAR and ELINT fields since 2006 after the required technique with several technical experiment satellites launch and operational test. ELINT satellites transmit data from satellite to earth station in real time with construction space-based network around it. Those data are simultaneously delivered to Anti-Ship Ballistic Missile(ASBM) connected land-based C4ISR network for marine target attack. Therefore China has enhanced surveillance and attack capability to the surrounding marine nations with space-based network around it. In the future, It is considered that China will increase accurate location search, signal processing and analysis ability through a further study on its technology.

• Bulletin of the Korean Space Science Society
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• 2010.04a
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• pp.29.1-29.1
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• 2010

GPS(Global Positioning System)로 대표되는 위성항법시스템(GNSS: Global Navigation Satel lite System)은 우주공간의 위성을 이용하여 사용자에게 위치와 함께 시각 정보를 제공해 준다. 위성항법시스템은 항법 분야 뿐 아니라 측량, 측지를 비롯하여 정밀 시각동기 및 지각변동의 측정까지 다양한 분야에서 활용되고 있다. 항법분야에 있어서 위성항법시스템의 오차를 제거한 정밀한 위치 정보를 이용하여 이동체에 활용하는 연구가 활발히 진행되고 있다. 위성항법을 움직이는 이동체에 적용할 경우 주변 환경에 따라 위성항법 신호의 오차가 증가하여 급격한 위치 오차를 유발하므로 추가적인 센서 사용을 통하여 안전성을 향상시킬 필요가 있다. 이 논문에서는 위성항법 기반의 위치정보와 이동체에 부착되어 있는 센서 정보를 병렬적으로 사용하는 주행시스템을 구성하고 주행 시험을 수행하였다. 이동체에 부착되어 있는 센서 정보를 이용한 주행시스템의 경우 이동 거리를 측정할 수 있는 엔코더와 조향각을 측정할 수 있는 포텐셔미터 그리고 차량 모델을 이용하여 구성하였다. 시험 결과 위성항법기반의 위치 정보와 이동체의 센서 정보를 이용한 위치 오차의 차이는 0.4m 이내로 위성항법 신호에 급격한 오차가 들어오는 경우 이동체의 센서 정보를 이용하여 감지할 수 있음을 확인하였다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2014.10a
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• pp.277-279
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• 2014

TEQC는 인공위성으로부터 수신한 데이터를 편집, 품질검사, 포맷변환하기 위한 소프트웨어이다. TEQC 품질검사를 사용하면 여러 결과파일이 생성되는데 이를 활용하여 DGPS기준국 전파수신 환경을 분석하였다. 특히 방위각, 앙각에 따른 장애물의 여부를 가능하다.

• Electronics and Telecommunications Trends
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• v.14 no.2 s.56
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• pp.125-126
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• 1999

디지털 위성방송 송신시스템은 27MHz/Ku 대역 위성방송 중계기를 통하여 4채널 이상의 NTSC급 TV신호와 2Mbps까지의 전송률을 가지는 데이터 신호를 프로그램 공급자로부터 일반 가정으로 공급할 수 있는 전송 시스템이다. 이 시스템은 '93년부터 ETRI와 캐나다 MPR Teltech사/LG정보통신과 공동으로 개발하기 시작하여 '95년도에 개발 완료하였으며, KBS/한국통신은 개발 시스템을 이용하여 '96년 6월부터 시험방송을 시작하였다.

• Information and Communications Magazine
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• v.26 no.6
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• pp.30-36
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• 2009

본고에서는 위성을 이용하여 WiBro(Wide Broadband)서비스를 제공하는데 있어서 WiBro 신호를 위성중계기를 통해 송수신할 경우, OFDM(Orthogonal Frequency Division Multiplexing) 신호가 갖고 있는 높은 PAPR(Peak-to-Average Power Ratio) 특성으로 인해 발생할 수 있는 전력증폭기의 비선형왜곡 현상에 대해서 기술하였다. 그리고 이를 효과적으로 극복할 수 있는 여러 방법들을 소개하고 모의실험을 통해 그 유효성을 확인하였다.

• Journal of Satellite, Information and Communications
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• v.8 no.4
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• pp.159-163
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• 2013

In this paper, we propose a new method to deinterleave multi-stage stagger PRI signals of pulse radars using the electronic intelligence systems. While former algorithms were based on hardware PRI tracker only using the first deviation of the TOA of radar signals, this paper uses the first and the second deviation of TOA of radar signals and uses the PRI histogram method to deinterleave multiple PRIs of pulse radars. This algorithm can be used for deinterleaving various PRI signals at electronic intelligence systems.

• Journal of Satellite, Information and Communications
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• v.7 no.2
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• pp.104-109
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• 2012

Currently, GPS(Global Positioning System) is used to find user location information. However, in some cases, especially in urban environments, we receive unreliable location information deu to multipath fading. In order to resolve this problem, we propose a closely coupled positioning technique where GPS signal is combined with QZSS signal. Also we proposed and analyze a combining algorithm of GNSS and Wi-Fi signals to get closely coupled location information by referring AP information. Finally, this paper proposes a combined GPS/QZSS/Wi-Fi navigation algorithm to improve navigation performance, and it is verified by testing of car deriving according to availability and accuracy standard.

• Aerospace Engineering and Technology
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• v.3 no.1
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• pp.109-116
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• 2004

In a satellite time management system, the GPS-based clock synchronization technique[1] has the merits of precision time management by knowing the time difference or the error between the OBT(On Board Time) of the internal processors and GPS time every second. It can be realized employing the DPLL(Digital Phase Loop Lock) and FEP(Front End Processor) circuitry for the clock synchronization[2]. In this paper, a refined DPLL & FEP scheme is proposed to provide the precision, stability and robustness of the operation, which is to compensate the errors and noise of the GPS signal, and also to cope with the case when the GPS signal is lost due to several reasons. The simulation and HIL (Hardware In the Loop) test results using the FM(Flight Model) in the course of KOMPSAT-2(Korea Multi Purpose Satellite-2) design and development are illustrated to demonstrate the salient features of this methodology.

• Journal of Satellite, Information and Communications
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• v.9 no.2
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• pp.119-125
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• 2014

In this paper, we developed the signal generator of GNSS navigation signals and analysis the performance of DCO(Digitally Clock Oscillator) compensation algorithm for cumulative distance error thorough simulation. In general, To generate a GNSS signal calculates the Doppler and Initial Pseudorange by using the location information of the receiver and the satellite. The GNSS signal generator generates a signal by determine the carrier and code output frequency using the Doppler information which is calculated as a function of time. The output frequency of the carrier and code would be used the DCO scheme. At this time, It extract the bit and code information on a for each sample by accumulating the DCO. an error of Pseudorange is generated by the cumulative error of the DCO. If Pseudorange error occurs, so that the influence to and operation of the receiver. Therefore, in this paper, we implemented the accumulated error compensation algorithm of the DCO to remove the accumulated error components DCO thereof, Pseudorange accumulated error is removed through the experiment, it was confirmed to be a high accuracy can be operated.