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- W2349344705 abstract "Causes and evaluation methods of time synchronization error of FOG SINS/GPS integrated navigation system were studied.In the evaluation method,by examining the quantitative relationship between time synchronization error of integrated navigation system and steady-state estimation of longitudinal accelerometer bias by Kalman filter,an empirical formula was given.A semi-physical simulation was conducted with stable navigation data from a FOG SINS and simulated flight track.The simulation results indicate that the precision of proposed method is better than 80ms when the time synchronization error is 0.5s." @default.
- W2349344705 created "2016-06-24" @default.
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- W2349344705 date "2011-01-01" @default.
- W2349344705 modified "2023-09-23" @default.
- W2349344705 title "A Novel Evaluation Method for FOG SINS/GPS Integrated Navigation System" @default.
- W2349344705 hasPublicationYear "2011" @default.
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