IqbalFaisal1
DinHussamud1
HanSeungoh2
LeeByeungleul1*
-
(School of Mechatronics Engineering, Korea University of Technology and Education,
31253, Korea)
-
(Department of Robotics and Automation Engineering, Hoseo University, 31702, Korea)
Copyright © The Institute of Electronics and Information Engineers(IEIE)
Index Terms
MEMS, tuning fork, resonator
I. INTRODUCTION
With improved performances, low cost, and compact size, MEMS tuning fork (MEMS-TF)
structures are widely used as gyroscopes (1-3) and resonators (4-6). The MEMS-TF structures consist of two masses and are operated in anti-phase motion.
These masses can be either coupled mechanically or electrostatically.
In electrostatically coupled resonators, it is challenging to achieve perfect anti-phase
motion since the fabrication errors are inevitable, and it is almost impossible to
fabricate two masses with the same frequency (7). To overcome this issue, mechanically coupled resonators have been proposed (8-10). One of the issues with mechanically coupled structures are the unwanted in-phase
motion, which lies at a frequency lower than the required anti-phase frequency. Also,
with the fabrication errors, both of the resonant modes can be merged.
MEMS-TF structures are believed to have the advantage of resisting linear accelerations,
when operated in an anti-phase mode. However, structure asymmetry and spring unbalancing
caused by the fabrication errors make MEMS-TF vulnerable to linear accelerations.
The effect of acceleration sensitivity (g-sensitivity), on the performance of MEMS-TF
structures has been presented widely (7,9,11-14), so it is essential to reduce the effect of linear accelerations (g-sensitivity)
on these structures.
Several design approaches have been reported to improve the g-sensitivity of mechanically
coupled MEMS tuning fork structures, Singh (10,15) studied the effect of linear accelerations, showing that the frequency decoupling
ratio between the in-phase and anti-phase modes can improve the acceleration sensitivity.
To further improve the resistance to linear accelerations and increase the decoupling
ratios, different spring architectures are proposed, such as lever mechanism (16,17), z-beam coupling spring (18), diamond-shaped (19), circular-shaped (8,20), T-shaped (21), lozenge-shaped (22), and polygon-shaped (23). Most of the proposed spring architectures presented exhibit either large surface
area or wide etch cavities. The large size of the spring will increase the device
size, making it difficult to use in specific applications such as consumer electronics,
whereas the wide etch area will make these springs more prone to fabrication errors.
In this article, a new coupling spring architecture has been proposed to overcome
the previous spring designs' issues. The proposed design benefits with the miniaturization
and narrow etch cavity, making it more robust to the fabrication errors. The proposed
coupling spring always prioritizes the anti-phase motion by keeping the unwanted in-phase
motion at a higher frequency, providing robustness to linear accelerations.
II. THE DESIGN CONCEPT OF THE MEMS TUNING FORK RESONATOR
The MEMS tuning fork resonator's conceptual design, which can be modeled as two degrees
of freedom system, is shown in Fig. 1. The two identical masses, left mass $(M_{L})~ $and right mass$\left(M_{R}\right)$,
are anchored through the left and right spring, $K_{L}$ and $K_{R},$respectively.
Also, both the masses are mechanically coupled through coupling spring $K_{c}$ to
form a shared resonance. The coupled resonators shown in Fig. 1 can be modeled as a second-order spring-mass system as shown below:
Here, $M,C,$ and $K~$represent the mass, damping, and spring constant of the resonator,
and subscripts$R$and$L$represent the right and left sides.$F_{L}$ and $F_{R}$ are
the applied forces.
Eqs. (1) and (2) can be solved for the in-phase and anti-phase motions by assuming $
M_{L}=M_{R}=M, C_{L}=C_{R}=C$ given by
(6,19):
In this equation, $x_{an}=x_{L}- x_{R}$ is the anti-phase motion, $x_{in}=x_{L}+x_{R}$
is the in-phase motion, $\omega _{in}=$ $\sqrt{(K_{L}+K_{R})/M}$and$\omega _{an}=\sqrt{(K_{L}+K_{R}+4K_{c})/M}$represents
the in-phase and anti-phase resonant frequencies, and $Q_{an}=M\omega _{an}/c$and$Q_{in}=M\omega
_{in}/c$are the anti-phase and in-phase quality factors respectively.
From Eqs. (3) and (4), it is clear that the in-phase and anti-phase resonant modes depend on the polarity
of the applied force and the coupling spring. The design goal for the coupling spring,
as discussed above, is to have an anti-phase resonant frequency lower than the spurious
in-phase resonant frequency, occupying a small surface area and narrow etch cavity.
This can be achieved by the proposed anti-phase coupling spring architecture shown
in the Fig. 2.
The proposed anti-phase spring architecture is comprised of outer, inner, and torsional
arms. The outer arms are connected to the masses, $M_{L}$ and $M_{R}$. Meanwhile,
one side of the inner arms is anchored, while the other side is connected to the outer
arm through the torsional arm in a rotationally symmetric manner, constituting $180^{\circ}$
in relation to the center of the coupling spring. The deformation of the designed
spring during the lateral load and axial load is shown in the Fig. 2(a) and (c) respectively. During the lateral load the outer arms move in the opposite direction,
whereas the inner arms move in the same direction, in such a way that the torsional
arm rotates along the lateral axis. The rotation of the torsional arm lessens the
resistance for a low frequency anti-phase resonant mode. However, during the axial
load, both the outer arms bend in the same direction, whereas the inner arms bend
in the opposite direction. This opposite motion of the inner arm resist the motion
of the torsional arm, resulting in a high frequency in-phase resonant mode.
The proposed spring architecture prioritizes the anti-phase motion, providing resistance
to linear acceleration and robustness to fabrication imperfections with the narrow
cavity holes. Resonant modes of the designed MEMS-TF resonator utilizing the anti-phase
coupling spring architecture are shown in the Fig. 3.
III. FEM SIMULATIONS
The designed MEMS-TF resonator was investigated through FEM simulation using COMSOL
Multiphysics. The resonator was simulated as single-crystal silicon having a Young
modulus of 179GPa and poison ratio of 0.29. A triangular mesh with a minimum element
size of 0.1$\mathrm{\mu}m$ was used, consisting of 120 $\textit{K}$ triangular elements.
Frequency domain study was used to investigate (i) the anti-phase operation of the
proposed coupling spring and (ii) the effect of linear acceleration on the resonant
modes of the MEMS-TF resonator.
3.1. Anti-phase Operation
FEM simulations validated the mechanically forced anti-phase motion. Initially, a
balanced force of $0.2\mu N$ was applied to both the masses$M_{R}$ and $M_{L}$. The
force $F_{R}$ and $F_{L}$ are acting on $M_{R}$ and $M_{L}, $respectively, as shown
in Fig. 4(a).
The frequency response function along with the phase is shown in Fig. 5(a). It can be observed that both masses are displaced in the anti-phase, having a maximum
displacement of $3\mathrm{\mu}m$ at a resonant frequency of 29,760 $Hz$. This configuration
is standard among MEMS-TF resonators to achieve anti-phase motion, also called electrical
coupling or indirect coupling.
Fig. 5. The frequency response of the tuning fork structure (a) with balance actuation
($FL=-FR$), (b) frequency response of the tuning fork resonator when a single side
force is applied.
The frequency response of the tuning fork structure (a) with balance actuation ($FL=-
FR$), (b) frequency response of the tuning fork resonator when a single side force
is applied.
The MEMS fabrication errors are inevitable, causing mass imbalance, spring imbalance
or force imbalance to the tuning fork structure. To study the effect of imbalance
force and robustness to the fabrication errors, one of the force was set to zero;
i.e., $F_{R}=0$. This means that a single side force was applied to the MEMS-TF resonator.
The frequency response function for this configuration is shown in
Fig. 5(b). It can be observed that, the in-phase motion occurred at a higher frequency of 30,370
$Hz$. Here, it is worth mentioning that the anti-phase motion still dominants, having
a displacement of $1.5\mathrm{\mu}m$.
2. Effect of Linear Accelerations
To study the effect of linear acceleration, a balanced force of $0.2\mu N$ was applied
to both masses in opposite directions to actuate the MEMS-TF resonator differentially.
Furthermore, a linear force was applied along the x-axis i.e. along the direction
of actuation, as shown in Fig. 4(b). The linear force corresponds to a linear acceleration, ranging from $0G$ to $6G$,
where, $1G=9.8m/sec^{2}$.
The effect of linear acceleration on the anti-phase resonant mode is shown in the
Fig. 6(a). It can be observed that at $0G$ both the masses $M_{L}$ and $M_{R}$ had been displaced
by $3\mathrm{\mu}m$ due to the balanced differential force, whereas the overall differential
displacement of $6\mathrm{\mu}m$ was achieved. Furthermore, the displacement of both
the independent masses, as well as the overall differential displacement was evaluated
under the linear acceleration of $3G$ and $6G$. By linear fitting, it was observed
that the linear acceleration sensitivity of the independent masses, $M_{L}$ and $M_{R}$
were$- 6nm/G$ and $5nm/G$ respectively, whereas the differential sensitivity was $1.1nm/G$.
Fig. 6. (a) Linear sensitivity of the anti-phase mode, (b) linear sensitivity of the
in-phase mode.
The same procedure was followed to study the effect of linear acceleration on the
in-phase resonant mode, where the results are shown in the Fig. 6(b). It can be observed that at $0G,$ the net displacement i.e. both of the individual
masses as well as differential displacement was zero, due to balance differential
force. However, at high $~ G$, it was observed that the in-phase mode was more susceptible
to the linear accelerations. The individual masses had an acceleration sensitivity
of $89nm/G$, while the differential output corresponded to $76.4nm/G$. This shows
that the anti-phase mode is $69.45$ times more resilient to the linear acceleration.
IV. EXPERIMENTAL RESULTS
The equivalent electrical model and test method of the fabricated MEMS-TF resonator
is shown in Fig. 7(a), while the optical image of the fabricated device using the designed coupling spring
is shown in Fig. 7(b). The resonator was fabricated using three wafer stacked processes (i.e., device wafer,
via wafer, and cap wafer), with a device thickness of $30\mu m$ and vacuum-sealed
at $100\textit{mtorr}$.
Fig. 7. (a) Electrical modal and experimental setup, (b) optical photograph of wafer-level
vacuum packaged MEMS-TF resonator (captured by EMI PHEMOS-1000).
The resonator was actuated by electrostatic force with an $AC~ $ voltage of$v_{ac}=100mV_{pk}$
and a $DC$ polarization voltage of $V_{DC}=5V$. The drive circuitry generates the
differential signal; i.e., $V_{DP}=V_{DC}+v_{ac}$ and $V_{DN}=V_{DC}- v_{ac}$. The
sense current was converted to the sense voltage using a charge amplifier, and the
frequency response function (FRF) was computed through the Zurich instrument (MFLI).
4.1. Characterization
4.1.1. Differential Balance Force
The frequency response of the left mass and right mass with balance differential
force is depicted in Fig. 8, showing both the masses moving in anti-phase motion (i.e., 180˚ out of phase, with
an amplitude response of $40mV$ and $39mV$). The anti-phase resonant frequency was
$27,280Hz$. A comparison of simulation and experimental results depicted a phase error
of $19^{o}$ between the two masses. It was found that the phase error arises from
the parasitic feed-through signal, i.e. the drive signal has been coupled to sense
signal through parasitic capacitances. The phase error can be minimized by implementing
the feed-through cancellation scheme as discussed in (2).
Fig. 8. Anti-phase resonant mode with balance-anti-phase force.
4.1.2. Single Side Force
When actuated by the single side, the resonant masses' frequency response is shown
in Fig. 9. During the anti-phase motion, as shown in Fig. 9(a), it can be observed that the output voltage is almost halved of the amplitude, $18mV$,
compared to the differential actuation, since the force is halved, while the phase
error was measured to be $13^{\circ}$. Meanwhile, the in-phase motion was observed
at a higher frequency of $27,780Hz$, with an amplitude of $0.4mV$, as shown in Fig. 9(b). It is worth mentioning that, with the single side force, the in-phase mode is suppressed
by $97.7\,\,\mathrm{\% }$, while the coupling spring prioritizes the anti-phase motion.
Fig. 9. Frequency response of the MEMS-TF resonator with single side force (a) anti-phase
response, (b) in-phase response.
V. CONCLUSION
This study has successfully demonstrated a new coupling spring design for MEMS tuning
fork structures. The new coupling spring design provides perfect anti-phase motion
at a lower resonant mode while keeping the surplus in-phase resonant mode high. The
designed coupling spring has low etched cavities, making it more robust to fabrication
errors and small surface area, resulting in a wide range of device applications. The
FEM simulations were carried out to study the effect of linear accelerations and un-balanced
forces. The in-phase mode is more susceptible to the linear accelerations, showing
that the individual masses have an acceleration sensitivity of $89nm/G$, whereas the
differential output corresponds to $76.4nm/G$. This shows that the anti-phase mode
is 69.45 times more resilient to the linear acceleration. Furthermore, experimentally,
the designed coupling spring architecture suppresses the in-phase mode by 97 %.
Author Contributions: Conceptualization, Faisal Iqbal, Seungoh Han and Byeungleul
Lee; Formal analysis, Faisal Iqbal; Software, Faisal Iqbal and Hussamud Din; Experiment,
Faisal Iqbal; Supervision, Byeungleul Lee; Writing—original draft, Faisal Iqbal; Writing—review
and editing, Faisal Iqbal, Hussamud Din, and Byeungleul Lee.
ACKNOWLEDGMENTS
This work is supported by the R&D program of the Ministry of Trade, Industry, and
Energy (MOTIE)/Korea Evaluation Institute of Industrial Technology (KEIT). (10084665,
Development of IMU Embedded 6-axis, 10-axis compound navigation system integrating
highly reliable inertial measurement unit (IMU), Global Navigation Satellite System
(GNSS), Magnetometer, and altimeter for maned/unmanned aircraft).
This work was (partially) supported by the post-doc scholarship program of KOREATECH.
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Author
Faisal Iqbal received his B.S. degree in Telecommunication Engi-neering from University
of Engineering and Technology, Peshawar, Pakistan.
He received his MS and Ph.D. degree in Interdisciplinary Program in Creative Engineering
from Korea University of Technology and Education, Republic of Korea, in 2017 and
2020, respectively.
He is currently working as a Research Fellow at Queen’s University Belfast, United
Kingdom.
Previously, he worked as Postdoctoral researcher at Korea University of Technology
and Education for 1 year. His research interests include MEMS based inertial sensors.
Hussamud din received his B.S. degree in Electronics Engineering from International
Islamic University, Islamabad, Pakistan in 2011, and M.S. degree in Electrical Engi-neering
from Center for Advanced Studies in Engineering, Islamabad, Pakistan in 2016.
He is currently pursuing his Ph.D. degree in Mechatronics Engineering at Korea University
of Technology and Education, Cheonan, South Korea.
His research interests include MEMS inertial sensors and energy harvesters.
Seungoh Han received his B.S., M.S., and Ph.D. degrees in electrical engineering at
Korea University (Seoul, Korea) in 1996, 1998, and 2006, respectively.
Since 2007, he has been working for Hoseo University (Asan, Korea) as a professor.
His current research interests include smart sensors, MEMS/NEMS, and coupled-physics
analysis of micro/nano-devices.
Byeungleul Lee is Professor at Korea University of Technology and Education.
He received his B.S. degree in Electronics Engineering from the Hanyang University,
and M.S. degree in Electrical and Electronics engineering from Korea Advanced Institute
of Technology in 1989 and 1991, respectively.
He obtained his Ph.D. in Electrical Engineering and Computer Science from the Seoul
National University in 2004.
From 1991 to 2008, he worked for Samsung Electronics as a principal researcher for
MEMS development. His research interests include semiconductor transducer and MEMS
applications.