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- W2394005471 abstract "A scheme of estimating the flight attitude of a rolling missile based on square root-unscented Kalman filter(SR-UKF)was proposed.To get the attitude of an experimental missile,a telemetry scheme based on two-axis liquid-droved rate gyroscope was studied.The telemetric data was processed by SR-UKF to reconstruct the attitude of missile.Aiming at the non-linearity of dynamic model of rolling missile,the scheme of attitude estimation algorithm based on square root-unscented Kaman filter(SR-UKF) was used to eliminate the errors caused by linearization of extended Kalman filter(EKF).Using the dynamic attitude model of low rate rolling missile,agroup of iterative filter equations based on SR-UKF were educed.The estimation result obtained form the proposed algorithm was compared with EKF and UKF ones,which showed the effectiveness of the proposed algorithm." @default.
- W2394005471 created "2016-06-24" @default.
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- W2394005471 date "2010-01-01" @default.
- W2394005471 modified "2023-09-23" @default.
- W2394005471 title "Estimation of the Attitude of a Rolling Missile Based on Square Root-unscented Kalman Filter" @default.
- W2394005471 hasPublicationYear "2010" @default.
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