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                                                 Resonant Micromechanical Systems

                              280   Chapter Five
                                        drive axis               drive axis

                              sense axis
                                                                                     sense axis
                                                               sense axis
                                                       sense axis

                                                drive axis                             drive axis







                                    input axis                       input axis

                                               (a)                              (b)
                              Figure 5.53 Classical tuning-fork microsensors: (a) out-of-the-plane driving; (b) in-plane
                              driving.

                                      mx ˙˙ + k x = F sin( Ȧ t)  m(y ˙˙ +2 Ȧx ˙ ) + k y =0
                                            d     0      d                   s          (5.143)
                              The particular solution to the first of Eqs. (5.143) is of the form:
                                                     x = Xsin(Ȧ t)                      (5.144)
                                                                d
                                                      p
                              where the amplitude is
                                                             F 0
                                                     X =                                (5.145)
                                                                2
                                                         k (1 íȕ )
                                                          d
                                                                d
                              with ȕ d  being the frequency ratio. Similarly, the particular solution of
                              the second of Eqs. (5.143) is of the form:
                                                     y = Y sin(Ȧ t)
                                                      p         d                       (5.146)
                                                                2
                                                             2Ȧ F 0
                              with               Y = í                                  (5.147)
                                                                2
                                                                       2
                                                       k k (1 íȕ )(1 íȕ )
                                                        d s
                                                                       s
                                                                d
                              When the sense amplitude Y is known, the input angular frequency can
                              be determined from Eq. (5.147).
                                This model characterizing the dynamic response of a single tine can
                              be utilized to evaluate the behavior of the two tines whose conjugate
                              motion can be monitored  electrostatically  or  by optical means.



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