메뉴 건너뛰기
.. 내서재 .. 알림
소속 기관/학교 인증
인증하면 논문, 학술자료 등을  무료로 열람할 수 있어요.
한국대학교, 누리자동차, 시립도서관 등 나의 기관을 확인해보세요
(국내 대학 90% 이상 구독 중)
로그인 회원가입 고객센터 ENG
주제분류

추천
검색

논문 기본 정보

자료유형
학위논문
저자정보

권건섭 (충북대학교, 충북대학교 대학원)

지도교수
유흥균
발행연도
2015
저작권
충북대학교 논문은 저작권에 의해 보호받습니다.

이용수6

표지
AI에게 요청하기
추천
검색

이 논문의 연구 히스토리 (2)

초록· 키워드

오류제보하기
The main mission of OTM(On-The-Move) satellite communication system is to provide satellite communication service while its platforms are moving. So it should have a capability to maintain a reliable communication channel when it travels at high speeds or in a severe fluctuation region. In addition, it needs to be small size and light weight to be installed on various vehicles.
In order to keep a reliable link, first, this paper proposes a simple multi-mode monopulse tracking system.
Conventionally, multi-mode monopulse tracking systems are applicable to large antenna systems such as fixed satellite earth stations due to their complexities in spite of their precision tracking performance.
This thesis presents a small multi-mode monopulse system applicable to the OTM satellite communication system which has only one mode coupler with a pair of slots using a feature of circular polarized received signal. Here, a tracking error signal is defined using fundamental and high-order modes before azimuth and elevation errors are derived from the amplitude and phase of the tracking error signal.
Also, in this thesis, a double-input single-output architecture of an LNA(Low Noise Amplifier) is presented to realize a light weight and small system suitable to be mounted on vehicles. In spite of advantages of the double-input single-output architecture of an LNA such as the reduction of the number of physical channels, it results in a time-varying phase error between a fundamental mode path and a high-order mode path. This dissertation shows that the error can be corrected by adding pilot signals to the LNA and using signal processing, and also gives the measured data on the phase error correction.
An OTM terminal for the satellite communication uses an OTM satellite communication system mounted on a vehicle and offers satellite communication service while moving via the Ka band GEO(Geostationary Earth Orbit) satellite. Hence, it is necessary to measure channel characteristics of an OTM terminal in the operating areas and throughly analyze the measured data for improving the link availability of the system.
This dissertation describes channel characteristics in the operating areas of OTM terminals, which are kinds of slow fading from blockage environments. In order to analyze the channel characteristics, the communication channel between the Koreasat-5 and an OTM terminal is measured and recorded in downtown areas of Daejeon city, highway and national road environments, using the beacon signal of the Koreasat-5, and the measured data are statistically analyzed and then compared with one another.
The statistical evaluations of the satellite channel have been performed by using a probability density function and the Markov model and then average connection duration(ACD), average fade duration(AFD), and level crossing rate(LCR) of each environment are presented.
At last, an M&S(Modeling & Simulation) method using three dimensional geographic information is proposed as an alternative method of channel characterization.

목차

I. 서 론 1
II. OTM 위성통신 시스템 8
1. OTM 위성통신 시스템 개요 8
2. OTM 위성통신 시스템 안테나 13
3. OTM 위성통신 시스템 추적 방식 18
III. 다중모드 모노펄스 추적 시스템 21
1. 급전혼 조립체 23
2. 모노펄스 추적 오차 신호 분석 30
3. 비콘 신호 처리 38
IV. 추적 오차 신호의 위상보정 방안 45
1. 저잡음 증폭기의 출력채널 단일화 구조 46
2. 파일럿 신호를 이용한 위상보정 방안 50
3. OTM 위성 통신 시스템 성능 측정 59
V. Ka 대역 OTM 위성단말 채널특성 70
1. Blockage 환경 분석 71
2. 3D 지형정보를 이용한 Blockage 환경 분석 100
VI. 결 론 116
참 고 문 헌 119

최근 본 자료

전체보기

댓글(0)

0