Input-output dynamics of the JPL microgyroscope

This paper discusses the identification of multi-input/multi-output models of the Jet Propulsion Laboratory (JPL) micromachined vibratory rate sensor (JPL microgyro). The sensor dynamics are accurately identified in the neighborhood of lightly damped degrees of freedom. Interesting features of the gyro are reported, including the presence of right-half-plane zeros. The results indicate that a multichannel lattice filter is suitable for adaptive sensor identification using test inputs of short duration to excite the sensor dynamics.

[1]  J. Nuttall Development of a solid-state gyroscope , 1990 .

[2]  J. Bernstein,et al.  A micromachined comb-drive tuning fork rate gyroscope , 1993, [1993] Proceedings IEEE Micro Electro Mechanical Systems.

[3]  M. W. Putty A Maicromachined vibrating ring gyroscope , 1994 .

[4]  Shyh-Biau Jiang,et al.  An unwindowed multichannel lattice filter with orthogonal channels , 1995, IEEE Trans. Signal Process..

[5]  V. Vorperian,et al.  Silicon Bulk Micromachined Vibratory Gyroscope , 1996 .

[6]  S. Youn,et al.  A surface-micromachined tunable microgyroscope , 1996, Proceedings 1996 IEEE Conference on Emerging Technologies and Factory Automation. ETFA '96.

[7]  Jonathan J. Bernstein,et al.  Micromachining inertial instruments , 1996, Photonics West - Micro and Nano Fabricated Electromechanical and Optical Components.

[8]  Barry Goldstein,et al.  Silicon bulk micromachined vibratory gyroscope for microspacecraft , 1996, Optics & Photonics.