• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.11 no.7
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• pp.1247-1257
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• 2000

Offset-fed dish antennas are considered. Offset-fed dish antennas are widely used for DBS reception, the problem of offset-fed dish antenna has, however, received little attention because of its complicated and asymmetric geometry. A Fourier-transform technique and Physical Optics are employed to express the fields radiated from offset-fed reflector and feed horn aperture. The simultaneous equations are solved to obtain a solution in a fast convergent series, thus facilitating the numerical computation. For given parameters such as diameter of reflector, focal length, offset height of reflector center, exact solutions are derived. Since offset-fed dish antenna has an application as multi-beam antenna using multiple feed, a brief feasablity of dual beam antenna for Korea-SAT (116$^{\circ}$E, EIRP 59 dBW) and Orion-SAT (139$^{\circ}$E, EIRP 54 dBW) is given in Conclusion.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.13 no.5
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• pp.484-491
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• 2002

This paper presents the results of a study of voltage-controlled PIN diode attenuators for Ku-band satellite payload and suggests the temperature-compensation method of these attenuators. The PIN diode attenuators are designed using thin-film hybrid techniques. The load resistance for maximum linear characteristics is determined by simulation and measurements. In the case of APD0805, load resistance of 150 $\Omega$ gives attenuator up to 10 dB linear attenuation range per a PIN diode. Also, measurements over temperature of these PIN diode attenuators were performed. From these measurements, designed PIN diode attenuators shows the severe temperature dependency due to forward voltage variation. A temperature compensation method using thermistor is now suggested to compensate the temperature variation of these PIN diode attenuators. This circuit shows good linear characteristics over wide temperature range

• Journal of Satellite, Information and Communications
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• v.3 no.2
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• pp.1-6
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• 2008

Space-time codes (STC) can achieve the diversity gain in a multi-path environment without additional bandwidth requirement. Recent study results reported that satellite systems can also achieve this diversity gain by using space-time codes in a cooperative network with terrestrial repeaters. Due to uni-directional nature of satellite DMB services, transmit diversity can be considered as one of the most effective ways to improve the performance. In this paper, we demonstrate various simulations results of STC schemes which can contribute to improve performance of future satellite DMB services. The STC schemes introduced in this paper provides diversity gains by combing independent coded signal from the satellite as well as from the terrestrial repeaters. In addition, we discuss a few points which should be considered to develop and implement these STC schemes.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.33 no.2A
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• pp.159-166
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• 2008

In this paper, we proposed an algorithm to solve the problem that can't maintain hop synchronization using only early-late gate tracking loop due to the drift of geo-stationary satellite in frequency hopping satellite communication system. When the signal is transferred to downlink through DRT(Dehop-Rebop Transponder), the problem with synchronization loss is occurred periodically when using only early-late gate tracking loop, because of energy loss in each side portion of hop due to orbital variation of the satellite. To solve this problem, we have developed Anti-Shrink synchronization tracking algorithm which uses the prediction value of transmission timing and the structure of inner-outer gate instead of early-late gate with the ranging information. Through simulations, we showed that the performance of the Anti-Shrink algorithm is better than that of simple inner-outer energy ratio algorithm and similar to that of conventional early-late tracking loop algorithm with ranging information. No synchronization failure in the proposed algorithm was occurred because of less energy loss and robustness without the ranging information.

• 한국정보통신설비학회:학술대회논문집
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• 2004.08a
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• pp.298-301
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• 2004

KT는 무궁화 3호 위성을 이용한 양방향 위성 통신 사업을 추진하고 있으며, 지상망을 이용하기 어려운 지역에 정부/공공, 에너지 산업, 기업 단일망 등 다양한 산업 분야를 대상으로 초고속 네트워크를 제공하고 있다. 양방향 위성 통신 서비스는 36,000km 상공의 위성 중계기와 지상 간의 통신 지연을 극복하기 위한 첨단 기술로 운용되고 있으며, 중요 데이터에 대한 위성 통신 품질보증 기능을 제공한다. 본 논문에서는 위성망의 트래픽을 수집하고 데이터를 로깅하는 위성망 트래픽 수집 도구와 수집된 데이터를 마이닝을 통해 실시간 모니터링하고 통계 정보를 생성하는 위성망 패킷 데이터 분석 도구로 이루어진 위성망 패킷 데이터 분석 시스템에 대해 논한다. 위성망 패킷 데이터 분석 시스템은 데이터 송수신 정보를 모니터링 함으로써 실시간 위성 통신 상태를 점검하고, 전송 지연 및 실패 등의 위성 통신 오류 상태를 조기 진단하고 조치할 수 있는 위성망 품질 보증 서비스를 제공한다.

• 전자공학회논문지 IE
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• v.45 no.1
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• pp.44-49
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• 2008

In this paper, the performance for the non-linear satellite channel including the characteristics of group delay and gain ripple of transponder is analyzed with multi-level QAM-OFDM schemes. Comparing the BER performances between general OFDM and CI(Carrier Interferometry)-OFDM for various QAM schemes, the degree of performance improvement is presented in AWGN environments for specified nonlinear characteristics. The simulations are performed with the 36MHz bandwidth of transponder channel and 120Mbps transmission rate for QPSK, 8QAM, 16QAM, 32QAM, 64QAM schemes between normal and worst case condition. It is shown that the improvement measure by the CI-OFDM for the group delay of channel and nonlinear characteristic of HPA outperforms that for the gain ripple in the case of higher level QAM scheme in normal condition. And the simulation results show that the additional techniques like the channel coding and compensation scheme against the nonlinear characteristic are required for 32QAM and higher level QAM in worst case condition.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.1
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• pp.72-78
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• 2015

Recently, the usage of the satellite is increased more and more in the areas that are communication, weather, marine, optical, radar etc. The functions of the Satellite are evolving from passive transponder to active transponder by the developing of a technology. Advanced countries in satellites install the DCAMP for increase of bandwidth efficiency, improvement of QoS by interference rejection. DCAMP includes many digital components in order to implement functions. Thus, these kinds of active transponders consume much more power compared to passive transponder and then increase the heat. In this paper, we discuss the TVAC test result of DCAMP in EQM(Engineering Qualification Model) level. The paper shows the test results of digital gain control in order to verify DCAMP status under the TVAC test. In addition, the temperature and heat condition of main components from viewpoint of derating will be treated through the official environment test for qualification.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• v.9 no.1
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• pp.1113-1116
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• 2005

Using COMSAT which provides multi-beam switching function, the optimal transmission channel environment which provides the high data rate communication are proposed in this paper. Also the link budget for communication transponder of COMSAT is designed. Based on the channel modeling for group delay, non-linear and gain flatness characteristics, the system performances which provide various data rate services were analyzed in Ka-band satellite channel. As the transmission data rate is increased, the degradation due to these channel characteristics is severely increased. The linear component of group delay and the AM-AM component of non-linear characteristics severely affect the system performance. To efficiently provide the various service via the same transmission system it is necessary to equalize the primary impairment factors. The optimum operating points of HDR satellite transmission system are implemented and operated by considering the analyzed results on channel characteristics.

• Electronics and Telecommunications Trends
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• v.21 no.4 s.100
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• pp.107-117
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• 2006

위성 탑재체 제조 산업은 기초 과학이 뒷받침된 초정밀 기계 공학, 첨단 전자 기술, 극한 환경 기술 및 신소재 공학 등과 같은 첨단 산업의 집합체라 할 수 있다. 현재 미국을 비롯한 서구 선진국에서 진행중인 탑재체 기술동향을 보면, 폭발적으로 증가하는 위성수에 따라 위성 궤도가 부족하고 주파수 자원이 고갈되고 있는 상황에서 통신 위성의 효율성과 성능을 향상시킬 수 있는 신호처리 탑재(OBP) 위성과 통신기능을 포함한 다양한 기능을 가진 복합위성 개발이 진행되고 있으며 주파수 대역의 포화와 광대역 멀티미디어 서비스 제공 등을 위해 보다 높은 주파수의 준 밀리미터파 대역(Ka 대역) 위성 개발이 활발히 이루어지고 있다. 국내에서는 현재, 2008년 발사를 목표로 마이크로스위치 매트릭스(MSM)가 탑재되어 빔간 스위칭이 가능하도록 설계된 통신해양기상위성(COMS)용 통신 탑재체(SACOM) 개발이 진행중이다. 국내의 위성탑재용 RF 부품분야는 1990년부터 위성 중계기 시스템의 기본적인 설계, 조립, 종합화, 시험기술을 바탕으로 통신위성 탑재체용 초고주파 부품을 개발하여 왔으며, 2000년대에는 Ku 대역(12/14GHz) 및 Ka 대역(20/30GHz) 기술인증모델(EQM) RF 부품을 성공적으로 개발하였다. 이를 바탕으로 통신해양기상위성 통신탑재체용 Ka 대역 RF 부품이 현재 우주인증 모델(QM)의 개발이 완료되었으며 비행 모델(FM) 개발이 진행중이다.

• Journal of Satellite, Information and Communications
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• v.1 no.2
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• pp.63-70
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• 2006

This paper presents the results of Ka band qualification model multiplexers for COMS Payload to be launched in 2008. These are the input and output multiplexers of the satellite transponder to use available frequency resources effectively and the diplexer of the satellite antenna to use the same reflector for both transmitting and receiving frequency bands, respectively. The input multiplexer with four frequency channels has four(4) independent channel filters which consist of an 8-pole elliptic band-pass filter for high frequency selectivity and a 2-pole equalizer for group delay equalization. For low insertion loss, mass and volume reduction, manifold type os employed for output multiplexer. E-plane T-junction is used for either splitting or combining a frequency band into two sub-bands. Asymmetric inductive irises are used to tune the receiving filter easily. The electrical performance and environmental test such as vibration test, mechanical shock test, thermal vacuum test and EMC test are performed and the results of all qualification model multiplexers are compliant to the requirement of each multiplexer. Followed by this qualification, the flight model equipment will be developed.