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8.3 Micromachined Gyroscopes                                                  203

                  results were reported for a structure 80 µm tall, operated at a low pressure (1
                  mTorr), which resulted in a quality factor for the oscillation of 1,000 to 2,000. This
                  was lower than expected and was attributed to anchor losses and voids inside the
                  polysilicon beams. Improved designs were expected to have a quality factor of up to
                  20,000. Similar to other micromachined gyroscopes, the resonant frequencies of
                  drive and sense mode were designed to be equal in order to amplify the sense mode
                  amplitude by the quality factor. Both resonant frequencies had a nominal value of
                  28.3 kHz. Any mismatch due to fabrication tolerances can be electrostatically tuned
                  by applying suitable voltages to the electrodes around the periphery of the ring. A
                  63-Hz mismatch was observed between the sense and drive modes, which required a
                  tuning voltage of only 0.9V. Other prototypes had a higher mismatch of up to 1 kHz
                  for which a tuning voltage of 6V was required to match sense and drive mode reso-
                  nant frequencies. The resolution of the device was measured to be less than 1°/sec
                  for a 1-Hz bandwidth; however, with some changes in the interface circuitry this
                  should be reduced to 0.01°/sec, which is then limited by the Brownian noise floor of
                  the structure.


                  8.3.2.2  Dual-Axis Gyroscopes
                  It is also possible to design micromachined gyroscopes that are capable of sensing
                  angular motion about two axes simultaneously. These devices are based on a rotor-
                  like structure that is driven into a rotary oscillation by electrostatic comb-drives.
                  Angular motion about the x-axis causes a Coriolis acceleration about the y-axis,
                  which, in turn, results in a tilting oscillation of the rotor. Similarly, any rotation of
                  the sensor about the x-axis causes the rotor to tilt about the x-axis. Conceptually,
                  this is shown in Figure 8.27.
                      An implementation of such a dual-axis gyroscope was reported by Junneau et
                  al. [67]. It was manufactured in a surface-micromachining process with a 2-m-thick
                  proof mass. The interface and control electronics were integrated on the same
                  chip. Underlying pie-shaped electrodes capacitively detect the tilting motion. To




                                                            z-axis drive









                          x-axis Coriolis
                          output oscillations                            y-axis Coriolis
                                                                         output oscillations




                                Input rate Ω X                          Input rate Ω Y
                  Figure 8.27  A dual-axis gyroscope. A rotor is driven into rotational resonance; angular motion
                  about the x- and y-axes causes the rotor to tilt, which can be measured capacitively by electrodes
                  below it. (After: [66].)
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