• 한국통신학회논문지
• /
• 제23권9A호
• /
• pp.2197-2210
• /
• 1998

In the grand alliance (GA) HDTV receiver, a coherent detection is empolyed for coherent demodulation of vestigial side-band (VSB) signal by using frequency and phaselocked loop(FPLL) operating on the pilot carrier. Additional phase tracking loop (PTL) employed to track out phase noise that has not been removed by the FPLL in theGA system. In this paper, we propose an algorithm for phase detection which utilizes a weighting function. The simplest implementation of the proposed algorithm using te sign of the Q channel component can be tractable by imposing a phase detection gain to the loop gain. It is obserbed that the propsoed algorithm has a robust characteristic against the performance of the digital filters used for Q channel estimation. A second goal of this paper is to introduce a gain control algorithm for the PTL in order to provide an effective implementation of the proposed phase detection algorithm. And we design the PTL through the realization of the simplified digital filter for H/W reduction. The proposed algorithms and the designed PTL are evaluated by computer simulation. In spite of using the simplified H/W structure, simulation results show that the proposed algorithms outperform the coventional PTL algorithms in the phase detection and tracking performance.

• 한국정보통신학회:학술대회논문집
• /
• 한국정보통신학회 2018년도 추계학술대회
• /
• pp.357-358
• /
• 2018

추적 레이더는 표적을 추적하기 위해 각도, 거리 및 주파수 추적루프를 사용한다. 특히, 레이더의 거리 추적루프 대역폭은 신호대 잡음비 및 표적의 거리에 따라 타협된 값으로 결정될 수 있다. 반면에 전자전은 레이더가 표적을 추적하지 못하도록 전자공격을 수행한다. 이때 전자전은 레이더의 추적루프 방해를 위해 기만 및 잡음재밍이 수행될 수 있다. 전자전에서는 레이더의 거리추적 대역폭을 추정하여 전자공격에 이용할 수 있다. 이를 위해 레이더 수집변수를 활용하여 레이더 거리추적 대역폭을 추정하는 방법에 대해 연구하였다.

• 한국항공운항학회지
• /
• 제19권4호
• /
• pp.6-11
• /
• 2011

Launch of the first Quasi-Zentih Satellite System (QZSS) satellite, dubbed Michibiki, took place September 11, 2010 and technical and application verification of the satellite is being carried out. This paper presents the results obtained from processing of the L5 signal transmitted from the QZSS satellite. The QZSS L5 signal is collected in ETRI, Korea. And then, the acquisition and tracking are performed by the L5 software receiver implemented by ETRI. The tracking loop of FLL, PLL, and DLL, the EPL correlator output, and the C/No output results show that the QZSS L5 signal is normally processed. Finally, the paper demonstrates that the QZSS L5 signal could be used as GPS satellite based augmentation system in Korea as well as Japan.

• 한국군사과학기술학회지
• /
• 제13권4호
• /
• pp.569-576
• /
• 2010

Jamming simulator has developed for the purpose of the test and evaluation on the electronic protection capabilities of the tracking radar onboard ship. This simulator has the capabilities to generate and radiate the jamming signals against the radar as well as those to receive, analyze and identify the radar signals at a real sea environment. The limited space of ship superstructure has led to the serious distortion caused by the ring around phenomenon that some sidelobes of the jamming beams were coming back to the receiving antenna. In this paper, we have proposed the methods to eliminate the ring around. First, we have inserted the groove metal screen between transmitting and receiving antennas. Second, we have used the PRI(Pulse Repetition Interval) tracking loop to control the switching timing of the input radar and the output jamming signal. Finally, we have demonstrated the performance and effectiveness of the proposed methods through the sea trial.

• 제어로봇시스템학회논문지
• /
• 제22권11호
• /
• pp.977-983
• /
• 2016

This paper proposes a novel code-tracking scheme to track the fine code synchronization for BOC (pn,n)-modulated global navigation satellite system signals in a repeat-back jamming environment. The correlation function of BOC (pn,n)-modulated signals has several peaks. The correlation function in the advanced offset region remains almost unchanged due to the repeat-back signals being received later than a line-of-sight signal in the same multipath signal receiving case. Additionally, the combined pseudo-random noise signal can be treated as repeat-back jamming signals, like multipath signals. In this paper, we propose a novel code-tracking scheme utilizing the advantages of using a combined pseudo-random noise signal in the advanced offset region and verify its performance through simulation.

• 한국항공운항학회지
• /
• 제19권2호
• /
• pp.23-28
• /
• 2011

Michibiki is the first QZSS satellite, which was launched by a H-IIA rocket departing from the Tanegshima in Japan on 11 September, 2010 and now operated successfully. This paper presents the results obtained from processing of the L1 C/A signal transmitted from the QZSS satellite. The acquisition and tracking are performed by the L1 software receiver implemented by ETRI. The signal processing results show that QZSS L1 C/A signal is normally processed through the tracking loop results of FLL, PLL, and DLL, the EPL correlator output, and the C/No output. Finally, the paper demonstrates that the QZSS satellite could be used in the navigation system together with the GPS satellite in Korea.

• 한국통신학회논문지
• /
• 제36권9C호
• /
• pp.581-588
• /
• 2011

본 논문에서는 cosine 위상 binary offset carrier (BOC) 신호를 위한 코드 추적 기법을 제안한다. BOC 자기상관함수는 다수의 부상관함수들로 이루어져 있으며, 본 논문에서는 이러한 부상관함수들을 재결합함으로써 주변첨두가 없는 새로운 상관함수를 획득한다. 마지막으로 delay lock loop 에서 사용되는 자기상관함수를 제안한 상관함수로 대체함으로써 주변첨두로 인한 false lock 문제를 해결한다. 또한 모의실험 결과를 통해 제안한 기법이 기존의 기법에 비해 더 좋은 tracking error standard deviation (TESD) 성능을 가지는 것을 보인다.

• 전력전자학회논문지
• /
• 제17권5호
• /
• pp.423-430
• /
• 2012

An adaptive maximum power point tracking (MPPT) scheme employing a variable scaling factor is presented. A MPPT control loop was constructed analytically and the magnitude variation in the MPPT loop gain according to the operating point of the PV array was identified due to the nonlinear characteristics of the PV array output. To make the crossover frequency of the MPPT loop gain consistent, the variable scaling factor was determined using an approximate curve-fitted polynomial equation about linear expression of the error. Therefore, a desirable dynamic response and the stability of the MPPT scheme were maintained across the entire MPPT voltage range. The simulation and experimental results obtained from a 3 KW rated prototype demonstrated the effectiveness of the proposed MPPT scheme.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2005년도 ICCAS
• /
• pp.1771-1774
• /
• 2005

Recently, RFID has become popular in the field of remote sensing applications. Location awareness is one of the most important keys to deploying RFID for advanced object tracking. Generally, multiple reference RF stations or additional sensors are used for the location sensing with RFID, but, particularly in indoor environments, spatial layout and cost problems limit the applicability of those approaches. In this paper, we propose a novel method for location sensing with active RFID systems not requiring the need for reference stations or additional sensors. The system triangulates the position of RF signal source using the signal pattern of the loop antenna connected to the power detector. The power detector consists of a signal strength detector and a signal analysis unit. The signal analysis unit indicates the signal strength and serial number using the signal from the strength detector, and provides the direction of the signal to the application target. We designed three different signal analysis units depending on the threshold type. The developed system can sense the direction to the transponder located over 10 m away within the maximum error of $5^{\circ}$. It falls within a reasonable range in our normal office environment.

• 한국통신학회논문지
• /
• 제33권2A호
• /
• pp.159-166
• /
• 2008

본 논문에서는 주파수 도약 위성 통신 시스템에서 정지 궤도 위성의 드리프트로 인해 Early-Late gate 동기 추적 알고리즘으로는 흡 동기를 유지할 수 없는 현상이 발생하는 문제를 해결하기 위한 동기추적 알고리즘을 제안하였다. 위성에 탑재된 역도약-재도약 중계기를 통해 신호가 중계될 때, 위성의 드리프트로 인하여 수신된 홉의 양쪽 에지에서의 에너지 유실 때문에 Early-Late gate 동기추적 알고리즘을 사용했을 경우 홉 동기를 유지할 수 없는 현상이 발생한다. 그러한 문제를 해결하기 위해 기존의 Ranging 거리 정보를 사용한 Early-Late gate 홉 에너지를 비교하는 구조를 변형하여 Inner-Outer gate 홉 에너지를 비교하고 송신타이밍을 예측하여 동기를 추적하는 Anti-Shrink 알고리즘을 제안하였다. 시뮬레이션 결과, 제안된 알고리즘은 기존의 내부-외부 에너지비율 알고리즘보다 우수하고, Ranging 거리정보를 사용한 Early-Late gate 동기추적 알고리즘보다 성능은 유사하지만 Ranging 정보를 사용하지 않고도 에너지 손실이 적어 위성의 드리프트에 robust하게 동기유지가 가능하다.