NEW ARCHITECTURAL DESIGN OF A TEMPERATURE ROBUST MEMS GYROSCOPE WITH IMPROVED GAIN-BANDWIDTH CHARACTERISTICS
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[1] A. Kourepenis,et al. Error sources in in-plane silicon tuning-fork MEMS gyroscopes , 2006, Journal of Microelectromechanical Systems.
[2] A.M. Shkel,et al. Inherently robust micromachined gyroscopes with 2-DOF sense-mode oscillator , 2006, Journal of Microelectromechanical Systems.
[3] Sangkyung Sung,et al. Design and performance test of a MEMS vibratory gyroscope with a novel AGC force rebalance control , 2007 .
[4] A. Shkel. Type I and Type II Micromachined Vibratory Gyroscopes , 2006, 2006 IEEE/ION Position, Location, And Navigation Symposium.
[5] Farrokh Ayazi,et al. Micromachined inertial sensors , 1998, Proc. IEEE.
[6] Andrei M. Shkel,et al. Structural Design Trade-Offs for MEMS Vibratory Rate Gyroscopes With 2-DOF Sense Modes , 2007 .
[7] L. E. Costlow,et al. Common design techniques for BEI GyroChip quartz rate sensors for both automotive and aerospace/defense markets , 2003 .
[8] Tayfun Akin,et al. A high-performance silicon-on-insulator MEMS gyroscope operating at atmospheric pressure , 2007 .