Review of the gyroscope free strap-down inertial navigation system
暂无分享,去创建一个
[1] Zu Jing. Research on Attitude Optimization Algorithm of Projectile at All Accelerometers' Installation Errors Based on GFIMU , 2009 .
[2] Chen He. The Study of the Feasibiliby of Fuze Based on the Geomagnetism Turns-counting Sensor , 2001 .
[3] Wang Jin. Optimum technology for non-gyro micro inertial measuring unit , 2002 .
[4] Sou-Chen Lee,et al. An innovative estimation method with own-ship estimator for an allaccelerometer-type inertial navigation system , 1999, Int. J. Syst. Sci..
[5] Marcelo C. Algrain. Accelerometer-based platform stabilization , 1991, Defense, Security, and Sensing.
[6] Liu Guang-bin. Six-accelerometers Configuration Scheme for SINS , 2003 .
[7] Xiong Yong. The Nongyroscope Strap down Inertial Navigation Method for Trajectory Correcting Fuzes , 1999 .
[8] P. Varaiya,et al. Design of gyroscope-free navigation systems , 2001, ITSC 2001. 2001 IEEE Intelligent Transportation Systems. Proceedings (Cat. No.01TH8585).
[9] S. J. Merhav,et al. A nongyroscopic inertial measurement unit , 1982 .
[10] V. Krishnan. Measurement of angular velocity and linear acceleration using linear accelerometers , 1965 .
[11] Sou-Chen Lee,et al. Innovative estimation method with measurement likelihood for all-accelerometer type inertial navigation system , 2002 .
[12] Alfred R. Schuler,et al. Measuring Rotational Motion with Linear Accelerometers , 1967, IEEE Transactions on Aerospace and Electronic Systems.
[13] Huang Tao. The Method of Measuring the Projectile Rotating Speed with Sensors , 2002 .
[14] Shi Zhen. Accelerometer Allocation Scheme in Gyroscope Free Strapdown Inertial Navigation System , 2002 .
[15] Sou-Chen Lee,et al. Gyroscope Free Strapdown Inertial Measurement Unit by Six Linear Accelerometers , 1994 .
[16] A. King,et al. Measurement of Angular Acceleration of a Rigid Body Using Linear Accelerometers , 1975 .