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학술지 경사각을 갖는 관성 항법 시스템 초기 정밀 정렬의 오차 분석
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저자
조성윤
발행일
200806
출처
제어로봇시스템학회논문지, v.14 no.6, pp.595-602
ISSN
1976-5622
출판사
제어로봇시스템학회
DOI
https://dx.doi.org/10.5302/J.ICROS.2008.14.6.595
협약과제
08MC2900, 실내외 연속측위 기술개발, 최완식
초록
In this paper, performance of the initial alignment for INS whose attitude is not leveled is investigated. Observability of the initial alignment filter is analyzed and estimation errors of the estimated state variables are derived. First, the observability is analyzed using the rank test of observability matrix and the normalized error covariance of the Kalman filter based on the 10-state model. In result, it can be seen that the accelerometer biases on horizontal axes are unobservable. Second, the steady-state estimation errors of the state variables are derived using the observability equation. It is verified that the estimates of the state variables have errors due to the unobservable state variables and the non-leveling tilt angles of a vehicle containing the INS. Especially, this paper shows that the larger the tilt angles of the vehicle are, the larger the estimation errors corresponding to the sensor biases are. Finally, it is shown that the performance of the 8-state model excepting the accelerometer biases on horizontal axes is better than that of the 10-state model in the initial alignment by simulation.
KSP 제안 키워드
Initial Alignment, Rank test, Sensor biases, State Model, State variables, error covariance, estimation error, kalman filter, normalized error, observability matrix, state estimation(SE)