Observability Analysis of Four-position Alignment for Laser Gyroscope Strap-down Inertial Navigation System
In this paper, A laser gyroscope strap-down inertial navigation system (SDINS) error model with 12 system state parameters is derived, and the observability of SDINS is discussed by observability analysis of piece-wise constant system (PWCS) and observable degree analysis method based on the singular value decomposition (SVD). It is demonstrated that fourposition alignment can make the system completely observable, and all the system state parameters can be estimated by Kalman filter. The simulation indicates the efficiency of the analysis results.
SDINS SVD PWCS four-position alignment Kalman filter observability
Jingyu Cao Jianxun Tang Yu Wang Guo Wei
College of Opto-electric Science and Engineering National University of Defense Technology Changsha, China
国际会议
2011 International Conference on Electronics and Optoelectronics(2011电子学与光电子学国际会议 ICEOE 2011)
大连
英文
686-689
2011-07-29(万方平台首次上网日期,不代表论文的发表时间)