Abstract:
A vibrator includes: a vibrating body; a driving unit for causing the vibrating body to vibrate in a predetermined vibrating direction; and a driving monitoring unit for detecting vibration displacement in a driving direction of the vibrating body. Stabilization of vibration in the driving direction of the vibrating body is achieved by applying positive feedback control to the driving unit based on the state of the vibration displacement in the driving direction of the vibrating body detected by this driving monitoring unit. The driving monitoring unit is constructed and arranged so as to be provided in a barycentric region of the vibrating body to detect the vibration displacement in the driving direction of the barycentric region of the vibrating body.

Description:
BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The present invention relates to a vibrator used for an angular velocity sensor or the like. 
     2. Description of the Related Art 
     FIG. 4 illustrates a plan view of a conventional vibrator  2  constituting a conventional angular velocity sensor  1 . The vibrator  2  of the angular velocity sensor  1  shown in FIG. 4 includes a substrate  3  in which a support fixed unit  4 , comb-shaped driving fixed electrode units  5  ( 5   a ,  5   b ,  5   c ,  5   d ,  5   e ,  5   f ,  5   g ,  5   h ) and detecting fixed electrode units  6  ( 6   a ,  6   b ,  6   c ,  6   d ,  6   e ,  6   f ) are each disposed in a fixed manner on the top face thereof. A vibrating body  8  is connected to the support fixed unit  4  via support units  7  ( 7   a ,  7   b ). 
     The vibrating body  8  is spaced from the substrate  3 , is disposed so that it can vibrate, and is constructed by including driving beams  9  ( 9   a ,  9   b ,  9   c ,  9   d ), an outer frame  10 , comb-shaped driving movable electrode units  11  ( 11   a ,  11   b ,  11   c ,  11   d ,  11   e ,  11   f ,  11   g ,  11   h ), support units  12  ( 12   a ,  12   b ), detecting beams  13  ( 13   a ,  13   b ,  13   c ,  13   d ) that are coupling beams, an inner frame  14 , and comb-shaped detecting moveable electrode units  15  ( 15   a ,  15   b ,  15   c ,  15   d ,  15   e ,  15   f ). 
     That is, one end side of each of the driving beams  9   a  and  9   b  is commonly connected to the support unit  7   a , one end side of each of the driving beams  9   c  and  9   d  is commonly connected to the support beam  7   b , and the other end side of each of the driving beams  9   a ,  9   b ,  9   c , and  9   d  is commonly connected to the outer frame  10 . 
     This outer frame  10 , as described later, can vibrate in an X direction shown in FIG.  4 . The comb-shaped driving moveable electrode units  11  are each provided in the outer frame  10  so as to be interdigitated with and spaced from the corresponding comb-shaped driving fixed electrode units  11 . Pairs of the driving fixed electrode units  5   a ,  5   b ,  5   c , and  5   d  and the driving moveable electrode units  11   a ,  11   b ,  11   c , and  11   d  that correspondingly face each other constitute a first driving unit (driving unit), and pairs of the driving fixed electrode units  5   e ,  5   f ,  5   g , and  5   h  and the driving moveable units  11   e ,  11   f ,  11   g , and  11   h  constitute a second driving unit (driving unit). 
     The support units  12   a  and  12   b  are each formed in the outer frame  10  so as to extend towards the inside of the outer frame  10 . Furthermore, the detecting beams  13   a  and  13   b  are each formed so as to extend from the end side of the support unit  12   a  while the detecting beams  13   c  and  13   d  are each formed so as to extend from the support beam  12   b.    
     The inner frame  14  is commonly connected to the extended edge side of each of the detecting beams  13   a ,  13   b ,  13   c , and  13   d . This inner frame  14  can vibrate integrally with the outer frame  10  in the X direction, as described below, and can also vibrate in a Y direction with respect to the outer frame  10 . The comb-shaped detecting moveable electrode units  15  are each provided in the inner frame  14  so as to be interdigitated with and spaced from the corresponding comb-shaped detecting fixed electrode units  6 . Pairs of the detecting fixed electrode units  6   a ,  6   b , and  6   c  and the detecting moveable electrode units  15   a ,  15   b , and  15   c  that correspondingly face each other constitute a first detecting unit (vibration detecting unit in the Coriolis force direction). Pairs of the detecting fixed electrodes  6   d ,  6   e , and  6   f  and the detecting moveable electrode units  15   d ,  15   e , and  15   f  constitute a second detecting unit (vibration detecting unit in the Coriolis force direction). Among a plurality of pairs of the detecting fixed electrode units  6  and the detecting moveable electrode units  15  that constitute the first and second detecting units, the pair of the detecting fixed electrode unit  6   c  and the detecting moveable electrode unit  15   c  and the pair of the detecting fixed electrode unit  6   f  and the detecting moveable electrode unit  15   f  constitute a driving monitoring unit. 
     A conductor pattern for supplying electric power from the outside to each of the driving fixed electrode units  5  and a conductive pattern for conductively connecting to each of the detecting fixed electrode units  6  are formed though they are not shown. 
     The vibrator  2  shown in FIG. 4 is constructed in the above-described manner. In this vibrator  2 , when an alternating driving voltage (driving signal) is applied between the driving fixed electrode units  5  and the driving moveable electrode units  11  that face each other, making use of elasticity of each of the driving beams  9 , the vibrator  8  vibrates (i.e., drive-vibrates) in the X-direction shown in FIG. 4, in which the support units  7   a  and  7   b  are caused to serve as fulcrums, in accordance with changes in the magnitude of electrostatic force based on the driving voltage. 
     In a state in which the overall vibrating body  8  is vibrated in the X direction in this manner, when the vibrating body  8  rotates about an axis in the Z direction (in the direction perpendicular to the drawing), the Coriolis force is generated in a direction, which is perpendicular to both the vibrating direction (X direction) of the vibrating body  8  and the center axis direction (Z direction) of rotation of the vibrating body  8 , that is, the Coriolis force is generated in the Y direction. This Y-direction Coriolis force causes the inner frame  14  of the vibrating body  8  to vibrate (i.e., detect-vibrate) in the Y direction relatively to the outer frame  10 , making use of the support units  12   a  and  12   b  as fulcrums and the elasticity of each of the detecting beams  13 . 
     By detecting the change in the capacitance between the detecting fixed electrode units  6  and detecting moveable electrode units  15  based on this Y-direction detecting-vibration, the magnitude of the angular velocity around the Z axis can be detected. 
     Normally, in order to avoid adverse effects such as air damping, the vibrator  2  is contained in a housing space defined by, for example, a glass member and is sealed in a depressurized state. In this case, the driving fixed electrode units  5  and the detecting fixed electrode units  6  of the vibrator  2  are constructed so as to be conductively connectable to the outside via a through-hole disposed in, for example, the glass member. 
     In FIG. 5, one example of a signal processing circuit connected to the vibrator  2  is shown along with main parts of the vibrator  2 . This signal processing circuit  20  is constructed by including a first detecting C-V converting unit  21 , a second C-V converting unit  22 , a summing amplifying unit  23 , a differential amplifying unit  24 , an AGC (Auto Gain Control) unit  25 , a phase inverting unit  26 , and a synchronous detecting unit  27 . In FIG. 5, the driving fixed electrode units  5 , the detecting fixed electrode units  6 , the detecting movable electrode units  15  and the vibrating body  8  of the vibrator  2  are illustrated in a simplified manner so that the construction of the signal processing circuit can be easily described. 
     The first detecting C-V converting unit  21  has a construction for converting the total capacitance between the detecting fixed electrode units  6  ( 6   a ,  6   b ,  6   c ) and the detecting moveable electrode units  15  ( 15   a ,  15   b ,  15   c ), which constitute the first detecting unit of the vibrator  2 , into a voltage and for outputting the converted signal. The second detecting C-V converting unit  22  has a construction for converting the total capacitance between the detecting fixed electrode units  6  ( 6   d ,  6   e ,  6   f ) and the detecting moveable electrode units  15  ( 15   d ,  15   e ,  15   f ), which constitute the second detecting unit, into a voltage and for outputting the converted signal. 
     When the vibrating body  8  vibrates only in the X-direction, the signal output from the first detecting C-V converting unit  21  is a signal A 1  having a waveform indicated by, for example, a dot-dash line A 1  in FIG.  6 A. The signal output from the second detecting C-V converting unit  22  is a signal A 2  having a waveform indicated by a dot-dash line A 2  in FIG.  6 B. The signal A 2  has the same amplitude and phase as those of the signal A 1  output from the first detecting C-V converting unit  21 . The phases of the signals A 1  and A 2  caused by these driving-vibrations are displaced 90° from the phase of a driving signal applied between the driving fixed electrode units  5  and the driving moveable electrode units  11  for causing the vibrating body  8  to vibrate. 
     In the example shown in FIG. 4, the detecting fixed electrode unit  6   a  and the detecting fixed electrode unit  6   b , the detecting moveable electrode unit  15   a  and the detecting moveable electrode unit  15   b , the detecting fixed electrode unit  6   d  and the detecting fixed electrode unit  6   e , and the detecting moveable electrode unit  15   d  and the detecting moveable electrode unit  15   e  have symmetric relationships, respectively. Hence, due to the driving vibration in the X direction, the change in the capacitance between the detecting fixed electrode unit  6   a  and the detecting moveable electrode unit  15   a  and the change in the capacitance between the detecting fixed electrode unit  6   b  and the detecting moveable electrode unit  15   b  are counterbalanced. Likewise, due to the vibration in the X direction, the change in the capacitance between the detecting fixed electrode unit  6   d  and the detecting moveable electrode unit  15   d  and the change in the capacitance between the detecting fixed electrode unit  6   e  and the detecting moveable electrode unit  15   e  are counterbalanced. 
     Because of this, when the vibrating body  8  driving-vibrates only in the X direction, the signal A 1  output from the first detecting C-V converting unit  21  responds to the change in the capacitance only between the detecting fixed electrode unit  6   c  and the detecting moveable electrode unit  15   c . The signal A 2  output from the detecting C-V converting unit  22  responds to the change in the capacitance only between the detecting fixed electrode unit  6   f  and the detecting moveable electrode unit  15   f . In other words, the vibration in the X-direction of the vibrating body  8  (driving direction) can be detected by the detecting fixed electrode units  6   c  and  6   f  and the detecting moveable electrode units  15   c  and  15   f  that constitute a driving monitoring unit. 
     When the inner frame  14  of the vibrating body  8  vibrates not only in the X direction but also in the Y-direction (Coriolis force direction) due to the angular velocity around the Z-axis shown in FIG. 4, the output signal from the first detecting C-V converting unit  21  is a signal obtained by overlapping the signal component A 1  due to the driving vibration and a signal component B 1  due to the angular velocity having the waveform indicated by a solid line B 1 . The signal component B 1  has the magnitude of the amplitude in accordance with the magnitude of the angular velocity. The signal components A 1  and B 1  are 90° out of phase. 
     When the angular velocity is generated, the output signal from the second detecting C-V converting unit  22  is a signal obtained by overlapping the signal component A 2  caused by the driving vibration and a signal component B 2  caused by the angular velocity having the waveform indicated by a solid line B 2  in FIG.  6 B. The magnitude of the amplitude of the signal component B 2  is in accordance with the magnitude of the angular velocity. In other words, the signal component B 2  has substantially the same magnitude of amplitude as that of the signal component B 1  of the output signal from the first detecting C-V converting unit  21 . The phase of the signal component B 2  is displaced by 90° from that of the signal component A 2  and is displaced by 180° from that of the signal component B 1  of the output signal from the first detecting C-V converting unit  21 . 
     In addition, there is a case in which the inner frame  14  vibrates caused by not only the angular velocity but also the acceleration in the Y direction. In this case, the output signal from the first detecting C-V converting unit  21  becomes a signal obtained by overlapping the signal component A 1  based on the driving vibration, the signal component B 1  caused by the angular velocity, and a signal component C 1  having the waveform indicated by a dashed line C 1  in FIG. 6A due to the acceleration. The magnitude of the amplitude of the signal component C 1  is in accordance with the magnitude of the acceleration and has the same phase as that of the signal component A 1 . 
     When the angular velocity and the acceleration are generated, the output signal from the second detecting C-V converting unit  22  becomes a signal obtained by overlapping the signal component A 2  based on the driving vibration, the signal component B 2  caused by the angular velocity, and a signal component C 2  having the waveform indicated by a dashed line C 2  in FIG.  4 ( b ) due to the acceleration. The magnitude of the amplitude of the signal component C 2  is in accordance with the magnitude of the acceleration. In other words, the magnitude of the amplitude of the signal component C 2  has substantially the same magnitude as that of the amplitude of the signal component C 1  of the output signal from the first detecting C-V converting unit  21 . The phase of the signal component C 2  is displaced from those of the signal component A 2  and the signal component C 1  by 180°. 
     In the above-described manner, the first detecting C-V converting unit  21  and the second detecting C-V converting unit  22  each output a signal in accordance with the vibration state of the vibrating body  8  to the summing amplifying unit  23  and the differential amplifying unit  24 . 
     The summing amplifying unit  23  applies summing-amplifying to the output signal from the first detecting C-V converting unit  21  and the output signal from the second detecting C-V converting unit  22 . Addition of the signal by this summing amplifying unit  23  causes the signal component B 1  of the output signal from the first detecting C-V converting unit  21  caused by the angular velocity and the signal component B 2  of the output signal from the second detecting C-V converting unit  22  to be counterbalanced and removed. Likewise, the signal component C 1  and the signal component C 2  caused by the acceleration are counterbalanced and removed. Because of this, the summing amplifying unit  23  outputs a signal in response to only a signal component, due to the driving vibration, obtained by adding the signal component A 1  and the signal component A 2  as a driving detecting signal (monitoring signal) to the AGC unit  25  and the synchronous detecting unit  27 . 
     The AGC unit  25  outputs the driving signal as a positive feedback control so that the vibrating body  8  stably vibrates in the driving direction at the resonant frequency based on the driving-detecting signal. Among the pair of the driving fixed electrode units  5  ( 5   a ,  5   b ,  5   c ,  5   d ) and the driving moveable electrode units  11  ( 11   a ,  11   b ,  11   c ,  11   d ) that constitute the first driving unit and the driving fixed electrode units  5  ( 5   e ,  5   f ,  5   g ,  5   h ) and the driving moveable electrode units  11 ( 11   e ,  11   f ,  11   g ,  11   h ) that constitute the second driving unit, the driving signal is applied directly into one of the driving units (the first driving unit in the example shown in FIG. 5) while the driving signal obtained by causing the phase inverting unit  26  to phase-invert the driving signal is applied to the other of the driving units. Application of this driving signal drives the vibrating body  8  into vibrating in the above-described manner. That is, in the vibrating body  8 , positive feedback control is applied to each of the first and second driving units based on the vibrating state of the vibrating body  8  in the vibrating direction (X direction) detected by the driving monitor unit, so that the vibration stabilization of the vibrating body  8  in the driving direction thereof is achieved. 
     The differential amplifying unit  24  obtains the difference between the signal output from the first detecting C-V converting unit  21  and the signal output from the second detecting C-V converting unit  22 . The differential of the signals of this differential amplifying unit  24  causes the signal component A 1  due to the driving vibration in the output signal from the first detecting C-V converting unit  21  and the signal component A 2  due to the driving vibration in the output signal from the second detecting C-V converting unit  22  to be counterbalanced. Because of this, the differential amplifying unit  24  outputs an angular velocity/acceleration mixed signal to the synchronous detecting unit  27  based on a signal component B 3 , indicated by a solid line B 3  in FIG. 7, obtained by subtracting the signal component B 1  from the 180° out of phase signal component B 2  due to the angular velocity, which results in the signal component B 1  being added to the signal component B 2  and a signal component C 3 , indicated by a dashed line C 3  in FIG. 7, obtained by subtracting the signal component C 1  from the 180° out of phase signal component C 2  due to the acceleration, which results in the signal component C 1  being added to the signal component C 2 . 
     The synchronous detecting unit  27  is integrated with a phase shifter (not shown), which causes the phase of the driving detecting signal output from the summing amplifying unit  23  to be displaced by 90° to generate an angular velocity reference signal. The angular velocity/acceleration mixed signal output from the differential amplifying unit  24  is synchronously detected making use of this angular velocity reference signal. 
     That is, the angular velocity reference signal is a signal whose phase is equal to or is displaced by 180° from that of the angular velocity component B 3  of the angular velocity/acceleration mixed signal. The synchronous detecting unit  27  integrates (synchronously detects) the angular velocity/acceleration mixed signal in a region D 1  of the phase of the angular velocity reference signal of 0° to 180° and in a region D 2  of the phase of the angular velocity reference signal of 180° to 360°. Since this synchronous detection removes the acceleration component C 3  of the angular velocity/acceleration mixed signal, the synchronous detecting unit  27  outputs a signal in accordance with the angular velocity component B 3  as the angular velocity signal. The magnitude of the angular velocity can be detected using this angular velocity signal. 
     In order that the outer frame  10  and the inner frame  14  of the vibrating body  8  ideally vibrate, the driving beams  9 , the outer frame  10 , the detecting beams  13 , the inner frame  14 , and the like that constitute the vibrating body  8  are preferably symmetric with respect to dashed lines A and B shown in FIG.  4 . However, since, from the point of view of machining accuracy, it is substantially impossible to make the driving beams  9 , the outer frame  10 , the detecting beams  13 , and the inner frame  14  in the above-described precisely symmetric manner, the driving beams  9 , the outer frame  10 , the detecting beams  13 , and the inner frame  14  become asymmetric. 
     When the acceleration in a Y-direction is applied to the vibrating body  8 , this asymmetry sometimes causes the vibrating body  8  to vibrate around, for example, an X-direction axis (i.e., to rotating-vibrate). When unwanted rotating-vibration is generated due to such acceleration, the capacitances between the detecting fixed electrode units  6   c  and  6   f  and the detecting moveable electrode units  15   c  and  15   f  that constitute the driving monitoring unit are changed due to not only driving-vibration of the vibrating body  8  caused by each of the first and second driving units, but also the influence of the unwanted rotating vibration caused by the acceleration. This leads to a state in which driving vibration signal components A 1  and A 2  of a signal output from the first C-V converting unit  21  and a second C-V converting unit  22  pick up noises caused by the acceleration. 
     Therefore, since the vibrating state of the vibrating body  8  in the driving direction cannot be accurately obtained, disturbance occurs in the positive feedback control of the driving vibration of the vibrating body  8 , which causes a problem in that driving vibration of the vibrating body  8  becomes unstable. When the driving vibration of the vibrating body  8  becomes unstable, the synchronous detecting unit  27  does not correctly generate a synchronous detecting reference signal, which leads to a problem in that an accurate angular velocity signal cannot be output. 
     SUMMARY OF THE INVENTION 
     The present invention is directed to solving the foregoing problems, and the object thereof is to provide a vibrator capable of preventing disturbance in the vibration of the vibrating body in the driving direction caused by an unwanted rotating vibration. 
     A vibrator in a first aspect of the invention comprises: a vibrating body; a driving unit for causing the vibrating body to vibrate in a predetermined vibrating direction; and a driving monitoring unit provided in a barycentric region of the vibrating body for detecting vibration displacement, in a driving direction of the vibrating body. 
     As a result, stabilization of vibration in the driving direction of the vibrating body is achieved by applying positive feedback control to the driving unit based on the state of the vibration displacement in the driving direction of the vibrating body detected by this driving monitoring unit, wherein the driving monitoring unit has a construction so as to be provided in a barycentric region of the vibrating body and to detect the vibration displacement in the driving direction of the barycentric region of the vibrating body. This construction serves as unit for solving the problems. 
     A vibrator in a second aspect of the invention is provided with the construction of the first aspect of the invention and is characterized in that the vibrating body has a construction in which flexible vibration can be obtained in the driving direction thereof and in a Coriolis force direction that is substantially perpendicular to the driving direction. A Coriolis force direction vibrating detecting unit for detecting the vibration displacement in the Coriolis force direction of the vibrating body is provided, and the angular velocity of rotation around a central axis having a direction perpendicular to both the driving direction and the Coriolis force direction is found based on the vibration in the Coriolis force direction of the vibrating body detected by the Coriolis force direction vibrating detecting unit. 
     A vibrator in a third aspect of the invention is provided with the construction of the first or second aspect of the invention and is characterized in that the vibrating body has a double-frame construction obtained by connecting an inner frame to the inside of an outer frame via a coupling beam so that the vibrating body can flexibly vibrate in the Coriolis force direction. The driving unit causes the outer frame and the inner frame to vibrate in an integral manner in the driving direction, and the inner frame has a construction so as to be vibrated in the Coriolis force direction with respect to the outer frame due to the Coriolis force caused by the angular velocity. The driving monitoring unit is provided in the barycentric region of the vibrating body disposed inside the inner frame while being supported by the inner frame. 
     According to this invention, since the driving monitoring unit is provided in the barycentric region of a vibrating body for detecting vibration displacement in a driving direction of the vibrating body, in other words, since, when the vibrating body unnecessarily rotating-vibrates, the driving monitoring unit is provided in the barycentric region of the vibrating body, which is the central part of the unwanted rotating vibration and which has a small vibration displacement, even though unwanted rotating vibration occurs, the noise caused by the unwanted rotating vibration picked up in the signal output from the driving monitoring unit can be maintained at a low level. 
     This can prevent disturbance in the positive feedback control of the vibrating body due to the unwanted rotating vibration, so that the vibration in the driving direction of the vibrating body by driving unit can be stably continued. 
     When the vibrating body flexibly vibrating in the driving direction as well as in the Coriolis force direction is provided and the angular velocity is detected based on the vibration displacement in the Coriolis force direction of the vibrating body, since the vibration in the driving direction of the vibrating body due to the unwanted rotating vibration can be prevented from being unstable in the above-described manner, the angular velocity can be substantially accurately detected regardless of occurrence of the unwanted rotating vibration. 
     In the vibrating body having a double-frame construction, since the construction of the vibrating body is complicated, unwanted rotating vibration tends to occur. Even though such unwanted rotating vibration occurs, since, as described above, the vibration in the driving direction of the vibrating body can be stably continued by reducing the adverse effect due to the unwanted rotating vibration to a small amount, in a case in which the vibrating body has the double-frame construction, it is particularly effective that the driving monitoring unit is provided in the barycentric region of the vibrating body. 
    
    
     For the purpose of illustrating the invention, there is shown in the drawings several forms which are presently preferred, it being understood, however, that the invention is not limited to the precise arrangements and instrumentalities shown. 
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a plan view illustrating one embodiment of a vibrator according to the present invention. 
     FIG. 2 is a graph showing the effect of this embodiment using experimental results. 
     FIG. 3 is a plan view illustrating another embodiment. 
     FIG. 4 is a plan view illustrating one example of a conventional vibrator. 
     FIG. 5 is a block diagram schematically illustrating one example of a signal processing circuit for detecting the angular velocity with the vibrator of FIG. 1 or FIG.  4 . 
     FIGS. 6A and 6B show waveform examples of signals output from a C-V converting unit shown in FIG.  5 . 
     FIG. 7 is an illustration showing waveform examples of signals output from a differential amplifying unit shown in FIG.  5 . 
    
    
     Other features and advantages of the present invention will become apparent from the following description of the invention which refers to the accompanying drawings. 
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     The embodiments according to the present invention are described below with reference to the drawings. 
     FIG. 1 shows one embodiment of a vibrator according to the present invention. This present embodiment is characterized in that driving monitoring unit is provided in a barycentric region of a vibrating body. Otherwise, the construction of the vibrator is the same as that of the conventional example of FIG.  4 . In the description of this embodiment, components that are identical to the corresponding components in the conventional example have the same reference numerals, whereby the repeated descriptions of the identical components are omitted. 
     In this embodiment, as shown in FIG. 1, comb-shaped detecting fixed electrode units  6  and detecting moveable electrode units  15  are provided in an opposed manner inside an inner frame  14  so as to be interdigitated with and spaced from each other to detect the vibration of the vibrating body  8  in the Coriolis force direction (the Y direction). Among these detecting fixed electrode units  6  and detecting moveable electrode units  15 , the detecting fixed electrode units  6  and the detecting moveable electrode units  15  within a barycentric region surrounded by a dashed line M shown in FIG. 1 function as the driving monitoring unit for detecting vibration displacement in a driving direction (X direction) of the vibrating body  8 . 
     As shown in FIG. 1, the driving monitoring unit is provided in the barycentric region M of the vibrating body  8  to detect the vibration displacement in the barycentric region M of the vibrating body  8  in the driving direction. 
     According to this embodiment, since the driving monitoring unit is provided in the barycentric region M of the vibrating body  8 , when the unwanted rotating vibration of the vibrating body  8  occurs due to the application of the acceleration in the Y direction, the disturbance of the driving vibration of the vibrating body  8  caused by the unwanted rotating vibration can be avoided. That is, even though the vibrating body  8  unnecessarily experiences rotating vibration due to the above-described application of acceleration and asymmetry, since the center of the unwanted rotating vibration is located in the barycentric region of the vibrating body  8 , the vibration displacement in the barycentric region M of the vibrating body  8  due to the unwanted rotating vibration is reduced to a small amount. 
     Therefore, even though the vibrating body  8  unnecessarily rotating-vibrates, by detecting the vibration displacement in the barycentric region M of the vibrating body  8  using the driving monitoring unit, the noise due to the above-described unwanted rotating vibration of the signal output from the driving monitoring unit becomes low. 
     As a result of this, normal positive feedback control is performed on the vibrating body  8 , which is hardly influenced by the occurrence of the unwanted rotating vibration, so that the driving vibration stably continues. Because of this, accurate angular velocity can be obtained regardless of the application of the acceleration. 
     The inventors of the present invention confirmed this from an experiment. In this experiment, a vibrator provided with the driving monitoring unit disposed in a region that is off the barycentric region M of the vibrating body  8 , as described in the conventional example of FIG. 4, was compared with a vibrator provided with the driving monitoring unit disposed in the barycentric region M of the vibrating body  8 , as shown in this embodiment. The comparison examined how the levels of the signal components (noises) that are caused by the unwanted rotating vibration (acceleration application) contained in the output signals from the synchronous detecting unit  27  shown in FIG. 5 differed between the two vibrators. The results of the experiment are shown in FIG.  2 . 
     In the graphs in this FIG. 2, the horizontal axis indicates the frequency of the acceleration applied to the vibrating body  8 , and the longitudinal axis indicates the level (acceleration sensitivity) of the noise caused by the application of the acceleration. The solid line α indicates the experiment result obtained by using the conventional vibrator provided with the driving monitoring unit disposed in the region that is off the barycentric region of the vibrating body  8 , and the solid line β indicates the experimental result obtained by using the vibrator according to the present embodiment provided with the driving monitoring unit disposed in the barycentric region M of the vibrating body  8 . 
     FIG. 2 demonstrates that, by providing the driving monitoring unit in the barycentric region M of the vibrating body  8 , as shown in this embodiment, the noise caused by the application of the acceleration can be considerably maintained at a low level compared to the conventional example. 
     As is shown in the above experimental results, by providing the construction in this embodiment, the noise caused by the application of the acceleration contained in the output signal from the synchronous detecting unit  27  can be maintained at a low level. Consequently, accurate angular velocity can be obtained. 
     This invention is not restricted to the above embodiment and can take various forms of embodiments. For example, in the above embodiment, though the vibrating body  8  has a double-frame construction constructed by connecting the inner frame  14  to the inside of the outer frame  10  via the coupling beams (detecting beams)  13 , the present invention can be applied to the vibrator provided with the vibrating body having a construction other than the double-frame construction. For example, it can be applied to the vibrating body in the embodiment shown in FIG.  3 . 
     In FIG. 3, components whose names are the same as in the above embodiment have the same reference numerals as in the above embodiment. The vibrator  2  shown in this FIG. 3 constitutes the angular velocity sensor in the same manner as in the above embodiment. The vibrating body  8  of the vibrator  2  is supported on a support fixed unit  4  using a support beam  30  formed by being folded into an U-shape and can vibrate in two directions, the X direction and the Y direction shown in FIG.  3 . By applying an alternating signal to the comb-shaped driving fixed electrode units  5  ( 5 A,  5 B), this vibrating body  8  driving-vibrates in the X direction in FIG. 3 due to change in the capacitance between the driving fixed electrode units  5  ( 5 A,  5 B) and the driving moveable electrode units  11  ( 11 A,  11 B). 
     During such a driving-vibration, by rotating around the Z-axis, the vibrating body  8  vibrates in the Y direction in FIG. 3 due to the Coriolis force caused by the rotation. This vibration displacement is detected as the change in the capacitance between the detecting fixed electrode units  6  ( 6 A,  6 B,  6 β,  6 β) and the detecting moveable electrode units  15  ( 15 A,  15 B,  15 α,  15 β), so that the angular velocity of the rotation around the Z-axis can be detected. In the example shown in this FIG. 3, pairs of the detecting fixed electrode units  6 α and  6 β and the detecting moveable electrode units  15 α and  15 β function as the driving monitoring unit. The positive feedback control is performed on the vibrating body  8  based on the vibrating state in the driving direction of the vibrating body  8  detected by this driving monitoring unit. 
     This driving monitoring unit is provided in the barycentric region of the vibrating body  8  in the same manner as in the first embodiment. This can prevent the disturbance in the driving vibration of the vibrating body  8  due to the acceleration application in the same manner as in the first embodiment. Even though the vibrating body  8  unnecessarily rotating-vibrates due to the acceleration application, the angular velocity can be substantially accurately detected. 
     In the above embodiments, although the description is made using the example of the vibrator embedded in the angular velocity sensor, this invention can be applied to the vibrator constituting a filter or the like. 
     While preferred embodiments of the invention have been disclosed, various modes of carrying out the principles disclosed herein are contemplated as being within the scope of the following claims. Therefore, it is understood that the scope of the invention is not to be limited except as otherwise set forth in the claims.