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학술지 정밀 항법 시스템 설계 및 알고리즘 검증
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저자
정성균, 김태희, 이재은, 이상욱
발행일
201303
출처
한국항공운항학회지, v.21 no.2, pp.8-14
ISSN
1225-9705
출판사
한국항공운항학회
DOI
https://dx.doi.org/10.12985/ksaa.2013.21.1.008
협약과제
13PR2500, 다원화 항법 주파수 감시 및 이용 기술 개발, 이상욱
초록
As GNSS(Global Navigation Satellite System) is used in various filed, many countriesestablish GNSS system independently. But GNSS system has the limitation of accuracy andstability in stand-alone mode, because this system has error elements which are ionosphericdelay, tropospheric delay, orbit ephemeris error, satellite clock error, and etc. For overcomeof accuracy limitation, the DGPS(Differential GPS) and RTK(Real-Time Kinematic) systemsare proposed. These systems perform relative positioning using the reference and userreceivers. ETRI(Electronics and Telecommunications Research Institute) is developingprecision navigation system in point of extension of GNSS usage. The precision navigationsystem is for providing the precision navigation solution to common users. If thistechnology is developed, GNSS system can be used in the fields which require precisionpositioning and control. In this paper, we introduce the precision navigation system andperform preliminary design and algorithm verification
KSP 제안 키워드
Algorithm verification, Clock Error, Real-time kinematic, Research institute, Satellite clock, Tropospheric delay, differential GPS, global navigation satellite system(GNSS), navigation system, preliminary design, relative positioning