지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2011.10
- 수록면
- 1,625 - 1,630 (6page)
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초록· 키워드
오류제보하기
In the ultra-tightly coupled GPS/INS integrated navigation system, the integrated Kalman filter plays the role of the signal tracking loop filters. This type of integration system is known to provide better navigation performance than other types of integration systems. In the ultra-tightly coupled system, the NCO commands are generated from the compensated SDINS output and calculated satellite position and velocity. In this paper, a method for generating NCO command is presented. In order to show the validity of the presented method a simulation system for an ultra-tightly coupled integrated navigation system was configured, in which a discriminator was used.
목차
Abstract
1. INTRODUCTION
2. ULTRA-TIGHTLY COUPLED GPS/INS INTEGRATED NAVIGATION SYSTEM
3. NCO COMMAND GENERATION FOR ULTRA-TIGHTLY COUPLED GPS/INS INTEGRATION METHOD
4. PERFORMANCE EVALUATION
5. CONCLUSION
REFERENCES
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UCI(KEPA) : I410-ECN-0101-2014-569-000915336