사파이어 (0001) 기판의 활성화 이온빔 (RIB) 처리 후 MOCVD에서 성장한 GaN박막의 열처리를 통한 구조 변화를 살펴보고, 전기적 성질의 변화를 관찰하기 위하여 전기로를 이용하여 열처리를 하였다. 시편의 분석을 위하여 DCXRD, Hall, TEM을 사용하였다. 1000˚C에서 시간을 변화시키면서 열처리한 시편에서 DCXRD의 FWHM는 약 50 arc-sec 정도 감소하였고, Hall 이동도는 약 80cm2/V.sec 정도 향상되었다. 가장 좋은 Hall 이동도를 보인 처리된 시편과 처리 전 시편의 TEM 비교 관찰에서 전위 밀도는 56~69% 정도 감소하였고 격자의 변형도 줄어들었다. 이것은 결정의 질과 전기적 성질 사이의 상관관계를 암시하며, 기판의 RIB 처리와 성장 후 적절한 열처리의 조합이 MOCVD로 성장시킨 GaN 박막의 특성을 개선시키는 것을 명확하게 보여준다.

본 논문은 초고주파 전력증폭기용 LDMOS(Lateral double-diffused MOS) MRF-21060소자의 게이트 바이어스 전압을 조절하여 온도 변화에 따른 드레인(Drain) 전류의 변화를 억제하기 위한 PNP 트랜지스터를 사용하여 능도 바이어스 회로 구현하였다. MRF-21060을 구동하기 위한 방법으로서는 AH1과 평형증폭기인 A11을 사용하여 구동 증폭단을 설계.제작하였다. 제작된 5W 초고주파 전력증폭기는 0~60℃까지의 온도변화에 대하여 소모전류 변화량이 수동 바이어스 회로에서 0.5A로 높은 반면, 능동 바이어스 회로에서는 0.1A이하의 우수한 특성을 얻었다. 전력증폭기는 2.11~2.17GHz주파수 대역에서 32dB 이상의 이득과 ±0.09dB이하의 이득 평탄도가 나타났으며, -19dB이하의 입.출력 반사손실을 가진다.

본 논문에서는 디지털 TV 중계기용 고출력 광대역의 3-Way 전력결합기를 설계.제작하였다. 대역폭 증가와 고출력을 동시에 이루기 위하여 Wilkinson 형태의 전력분배기를 채택하였다. 우선 Wilkinson 전력분배기를 균등(1 : 1) 및 비균등(2 : 1) 분배시켜, 동위상 4 포트 전력결합기를 시뮬레이션 하였다. 시뮬레이션 결과에 따라서 두께 120 mil인 유전체 기판을 사용하여 제작된 전력결합기는 디지털 TV 중계기 주파수 470~806 MHz 대역에서 삽입손실 -6.53dB 이하, 반사계수 -13dB 이하, 포트 간 분리도 -15 dB 이하, 출력 포트 간 위상차가 13˚이하의 특성을 보였다. 새롭게 만든 전력결합기는 회로에서의 고 임피던스로 인한 마이크로스트립 선로 폭의 한계와 고출력의 경우 선로간의 상호작용으로 인한 전력의 손실 및 협대역의 문제를 동시에 개선이 가능함을 알 수 있었다. 나아가서, 제작된 3-Way 결합기의 삽입손실, 반사계수, 포트간의 분리도 및 위상차가 디지털 TV 중계주파수 470~806 MHz에서 양호한 특성을 나타내는 것을 확인함으로써 고출력 및 광대역화가 실현가능하다는 것을 알 수 있었다.

황섬유의 최저손실 파장영역인 1.55μm에서 고출력으로 안정하게 농작하는 광센서용 광원인 반도체 레이저를 제작하기 위하여 이론적인 해석을 수행한 후 제작하였다. 활성영역과 SCH층의 재료는 Ln1-xGaxAsyP1-y를 사용하였다. 광센서용 광원으로 사용되기 위해서는 넓은 스펙트럼 폭을 가지며, 가간섭 길이가 짧은 특성을 가지는 조건을 만족해야 한다. 따라서, 반도체 레이저에서 레이징을 억제시켜 줌으로써 넓은 스펙트럼 폭을 가지도록 설계를 하였고, 광섬유와 결합효율을 높일 수 있도록 tapered 형태의 스트라입 구조를 채택하여 마스크 패턴을 형성하였다. 또한, 레이징을 억제하기 위하여 후면에 윈도우 영역을 두었고, 측방향으로 경사각을 두어 반사도를 낮추도록 설계 및 제작하였다. 7도와 15도의 측면 경사각을 가지는 구조와 굽은 스트라입 구조를 가지는 소자를 제작하여 특성을 측정한 결과, 광센서용 광원으로서 적용이 가능한 광출력 특성과 넓은 스펙트럼 폭을 가졌다.

본 논문에서는 DTV 중계기용 Temperature Independent Biasing을 이용한 100 watt급 단위 전력증폭기를 설계한 후, 제작하였다. 20℃에서 100℃까지의 온도변화에 대하여 단위 전력증폭기의 DC 동작점은 능동 바이어스에 의해서 고정되며, 증폭기의 소모전류의 변화량이 0.6A 이하의 우수한 특성을 얻었다. 제작된 단위 전력증폭기는 12dB 이상의 이득, ±0.5dB 이하의 이득 평탄도, DTV 중계 주파수범위(470-806 MHz)에 걸쳐 15dB 이하의 입.출력 반사손실을 나타내었다. 100 Watt 단위 전력증폭기는 출력 전력이 100 watt일 때 2MHz의 오프셋에서 32dBc 이상의 상호 변조 왜곡(IMD)을 나타내었다.

This paper describe the method and the result of making a fiber optic gyrocompass measuring the heading angles of a ship with a fiber optic sensor. As the method seeking for the heading angles, it is possible to get the heading angles by measuring the output signals from a stationary fiber optic sensor in at least three directions such as a heading direction and other two directions having phase difference Φ1 and Φ2 to the heading. We made the static fiber optic gyrocompass by a high performance fiber optic sensor having scale factor of 210mV/deg/s and resolution of 0.5deg/hr using this principle. The accuracy of this system was 0.29˚ from 20 numbers of data measuring the arbitrary heading angle.

The purpose of this reserch is the development of 406MHz satellite EPIRB terminals which is used on Cospas/Sarsat system. This equipment is essencial facility in all vessel due to should be equipped according to GMDSS. This 406MHz satellite EPIRB needs high technology of complicated. Because, this is designed to operate stably with ultra-stability oscillator and with the low power consumption so that can operate continually for 48 hours by the contained battery. The development of this equipment is significant in the sides of acquirement of new technology on satellite communication fields. In this research, we investigated the international and domestic regulations of needed. Because this equipment is international system concerned with life of man. So, we designed the adequate hardwares and softwares from this research. From this research, we developed the equipment with appopriate capability for productions, and much more research is needed to develop the more small size more chip one for production.

This is the first report about the development of INMARSAT-C Satellite communication terminal. We analyze the existing Inmarsat-C terminal and examine each rules(IMO rule, domestic rules) about terminal. With that result, we design the basic hardware and software of terminal. This report consists of ; 1) the contents of the overall of operating situation and resources of INMARSAT-C system as like operation of communication system, communication channels and services 2) the contents of the specification of Inmarsat-C terminal hardware and software and the rules of IMO and Type approval 3) the design of basic hardware and reserch of signal modulation/demodulation using Viterbi algorithm 4) the design of software algorithms and functions focused in korean situations.

In this study, a vertical type LPE system has been developed for III-V semiconductor compounds single crystal growth. On the basis of the experience & basic study using this system, the system modification has been carried out for a ultra thin multi-layer single crystal. The temperature fluctuation was within ±0.006℃ at 800℃, temperature uniformity for graphite boat around was within ±0.15℃ at 650℃, and cooling rate was controllable from 2.2℃/min to 0.05℃/min. As a result it is considered to satisfy the condition to grow a ultra thin layer single crystal of III-V semiconductor compounds.

Various types of optical gyroscopes have been proposed and researched to the present in the world. This paper provides an overview of the types of optical gyroscopes, and also introduces technical principles, characteristics, advantages and disadvantages for each type. Moreover, the critical problems in a design have been discussed.

Fiber optic gyroscopes must be a promising technology that can replace conventional mechanical ones based on the principle of inertia of spinning masses. The advantages of fiber optic gyroscopes over mechanical ones include low cost, light weight, compact size and fast turn-on time. We will apply them to fiber optic gyrocompass for ships. Fiber optic gyrocompass for ships requires the north-seeking accuracy of 15˚/hr, earth rotation rate, or better. This article introduces the fiber optic gyroscope as rotation sensor in the fiber optic gyrocompass system for ships that is planed to develop in our laboratory.

Shortening the lasing wavelength(particularly below infrared ; the visible region) of laser diodes is very attractive because it can provide a wide range of applications in the fields of optical information, measurement, sensor, the development of medical instrument, and optical communication through plastic fibers. According to the recent researches on the field, InGaAsP/GaAs was suggested as a material for red-light laser. In this study, in order to grow InGaAsP/GaAs epitaxial layer on InGaAsP/GaAs by LPE, we used GaP and InP two phase solution technique for 670nm and 780 nm region, respectively. Through the X-ray diffraction measurement for the epitaxial layer grown from the experiments, we found that the lattice mismatch of In0.46Ga0.54As0.07P0.93/GaAs and In0.19Ga0.81As0.62P0.38/GaAs was about +0.3% and +0.1%, respectively.

Since it is very important for an ocean-going vessel to transmit information quickly and accurately to her owner or charterer not only for the ship's safety but for economic operation of the ship, some newly-built automated vessels equipped with automatic information transmission system which consists of INMARSAT-C and specially-designed computer. This system, however, is not applicable to the existing vessel without chaging her equipments and, furthermore, is too expensive for small shipping companies to fit out such a system on their vessels. Therefore, we propose a low-priced information transmission system which consists of a personal computer and communication equipments in the existing vessel, and in this paper, as the groundwork of the proposed system, we have made up the ship's position transmission system which is composed of and IBM AT-compatible, PC, INMARSAT-A and a GPS receiver. As the test result of the system through sea trial on the training ship 'HANBADA', we confirmed that transmission of the ship's position was achieved succesfully and consequently there could be high possibility of cost-effectiveness of the proposed system

In order to grow InGaAsP epitaxial layer on GaAs by LPE, an accurate phase diagram for In-Ga-As-P quarternary compounds is required. But the short wavelength InGaAsP/GaAs phase diagram for full wavelength range was not yet reported. In this study, therefore, a theoretical calculation has been carried out by using thermodynamic's equation for InGaAsP/GaAs in order to get the relation between the mole fraction of the sloute and solid phase compounds. And the calculation being compared with the dta of Kawanishi et. al, the result has been shown that his phase diagram obtained by the calculation can apply to growing InGaAsP/GaAs by LPE.

In this paper the results for thin multi-layer InGaAsP(1.3μm)/InP crystal growth by vertical liquid epitaxial growing furnance have been presented. The growth rates of InGaAsP layer and InP layer at cooling rate of 0.3℃/min and the growing temperature of 630℃ were obtained as 0.11 μm/min and 0.06 μm/min, respectively, by the uniform cooling with two phase solution technique.