Various embodiment of the invention relate generally to a MEMS device with a proof mass and particularly to a MEMS device operable to measure ambient acceleration and ambient magnetic field by detection motion caused on the proof mass.
MEMS devices typically include sensors for measuring the motion of a proof mass, such as proof mass motion caused by an ambient acceleration and proof mass motion caused by an ambient magnetic field. Currently, a magnetometer, used for measuring the magnetic field is a device separate and apart from an accelerometer used for measuring ambient acceleration. However, due to fabrication imperfections or by design a magnetic field sensor can have a response to an ambient acceleration. A single MEMS device is proposed to measure both ambient acceleration and ambient magnetic field. This results in a smaller MEMS device by decreasing the MEMS footprint and therefore cost.
It is obviously desirable to reduce the size of the sensors and/or the number of required semiconductors in an effort to reduce cost and size.
Accordingly, there is a need for a small MEMS device with decreased costs and increased performance.
Briefly, an embodiment of the invention includes a MEMS device having at least one proof mass. A first magnetized magnetic material disposed partially on a surface of the at least one proof mass. A first spring anchored to a substrate to support the at least one proof mass. A first sensing element responsive to both ambient magnetic and ambient acceleration and a second sensing element coupled to the at least one proof mass. The at least one proof mass moves in response to ambient acceleration and ambient magnetic field. A configuration of the first and second sensing element comprising a signal processor, the signal processor operable to provide a first output responsive to ambient magnetic field.
A further understanding of the nature and the advantages of particular embodiments disclosed herein may be realized by reference of the remaining portions of the specification and the attached drawings.
a) and 2(b) show a couple of circuit configurations of the sensing elements in measuring acceleration and magnetic field.
a) and 3(b) show circuit configurations including switches that cause the different configurations.
The following description describes a MEMS device. The MEMS device has a proof mass and two sensing elements used to measure an ambient acceleration and an ambient magnetic field, as discussed below
Particular embodiments and methods of the invention disclose a MEMS device including a first proof mass, a first magnetized magnetic material disposed partially on a surface of the first proof mass, a first spring anchored to a substrate to support the first proof mass, and a first sensing element coupled to the first proof mass and operable to sense the motion of the first proof mass caused by an ambient acceleration. The MEMS device further includes a second sensing element coupled to the first proof mass and operable to sense the motion of the first proof mass caused by an ambient magnetic field. In the described embodiments, ambient magnetic field refers to any magnetic field other than the magnetic field created from the deposited magnetic material on the proof mass.
Referring now to
The proof mass 12 has a magnetized magnetic material 16 disposed on at least a part of the surface thereof, similarly, the proof mass 14 has a magnetized magnetic material 18 disposed on at least a part of the surface thereof. The sensing elements 20 and 22 are shown coupled to the proof mass 12 and the sensing elements 24 and 26 are shown coupled to the proof mass 14. The springs 28 and 29 are connected to anchors 30 and 32 and the anchors are fixed to the substrate, which lies under the structures shown in
In the embodiment of
In some embodiments of the invention, each of the magnetized magnetic materials 16 and 18 is not necessarily a solid piece and is rather made of smaller pieces, as shown in
In some embodiments of the invention, each of the magnetic materials 16 and 18 is made of or any combination of cobolt (Co), iron (Fe), and nickel (Ni).
In an embodiment of the invention, each of the sensing elements 20-26 is a variable capacitor. In another embodiment of the invention, each of the sensing elements 20-26 is a pieizoresistor sensing element, a piezoelectrical sensing element or an optical sensing element. In the embodiments and discussions to follow, the sensing elements 20-26 are assumed to be capacitors. It is understood that the same discussions and embodiments apply to embodiments with sensing elements 20-26 that are not capacitors.
Under ambient positive x-axis acceleration a counter-clockwise torque τa1 is imposed on the proof mass 12. The proof mass 12 rotates counter-clockwise and sensing element 20 increases and the sensing element 22 decreases.
Under ambient positive x-axis acceleration a clockwise torque τa2 is imposed on proof mass 14. Proof mass 14 rotates clockwise and sensing element 24 increases and the sensing element 26 decreases. Alternatively, one of the proof masses 12 or 14 may be employed with two sensing elements to measure the acceleration and magnetic field independently on one proof mass.
In measuring an ambient magnetic field, an ambient magnetic field By is applied to the MEMS device 10, of
Sensing is now discussed relative to
a) and 2(b) show a couple of circuit configurations of the sensing elements 20-26 for measuring external acceleration and external magnetic field where the sensing elements are variable capacitors like parallel plate electrodes or linear comb fingers.
In an embodiment of the invention, for sensing external x-axis acceleration, the sensing elements 20-26 are connected in a Wheatstone bridge configuration as shown in
In an embodiment of the invention, for sensing external x-axis magnetic field, the sensing elements 20-26 are connected in a Wheatstone bridge configuration as shown in
In an embodiment of the invention, Vin can be a combination of alternating current, DC or a combination of AC and DC. In an alternate embodiment, the terminals marked V0 can be connected to a differential transcapacitance amplifier. In this embodiment the output of the amplifier is proportional to the capacitance change of the sensing elements 20-26. In yet another embodiment, the driving voltage, Vo, can be applied to sensing elements 20-26 and the output signal can be detected from the proof mass nodes marked Vin, in
In an embodiment of the invention, a switch may be used to switch between the configurations of
By rotating the MEMS device 10, of
Circuit 300a shown in
In
As with the embodiment of
Under an external +z acceleration proof mass 402 will experience a negative RX torque τa1 causing proof mass 402 to rotate about axis 430 in the negative RX direction. Under an external +z acceleration proof mass 404 will experience a positive RX torque τa1 causing proof mass 404 to rotate about axis 430 in the positive RX direction. The motions due to the negative RX torque τa1 and positive RX torque τa1 are detected by sense elements 20-26 under the proof masses 402 and 404 using the circuit configuration in
Under an external negative z-axis magnetic field (Bz) the magnetic material 406 of MEMS device 400, interacts causing a torque τm1=V My×Bz on proof mass 402 causing the proof mass 402 to rotate about axis 430 in the positive RX direction. Under an external negative z-axis magnetic field (Bz) the magnetic material 408, of MEMS device 400, interacts causing a torque time τm2=V My×Bz on proof mass 404 causing the proof mass 404 to rotate about axis 430 in the positive RX direction. The motions due to the magnetic torques (τm1 and τm2) are detected by sense elements 20-26 under the proof masses 402 and 404 using the circuit configuration in
Magnetic self-test is useful both during manufacture and use. For z-axis magnetometers, flowing current can be used to generate a z-directed magnetic field.
The bridge 602 is analogous to the circuit configuration with switches of
In operation, out-of-phase voltage pulses are provided as input to the bridge 602 at 306 and 308. The output of bridge 602, analogous to circuit 300a and 300b, is converted to voltage by the amplifier 604 and the output of the amplifier 604 is converted from analog form to digital form. The resulting digital signal, i.e. the digital output by the ADC 606, is processed by digital electronics 608 to produce values for both acceleration and magnetic field.
In an alternative embodiment of the invention, the amplifier 604 is a differential trans-capacitance amplifier.
The MEMS device 700 is further shown to include a spring 710 and an anchor 712. The anchor 712 is connected to the substrate, which is under the structures shown in
Under acceleration in the positive y direction, proof mass 702 experiences a force in the negative y direction causing a linear motion of the proof mass 702 in the negative y direction. For a negative y displacement, in the case where the sensing elements 20-26, 714, and 716 are capacitors, capacitors 20 and 22 increase in capacitance and capacitors 24 and 26 decrease in capacitance. To sense acceleration, the positive-going capacitors in a bridge configuration such as in
Under a positive x-axis magnetic field the proof mass 702 experiences a negative z-axis torque causing the proof mass 702 to rotate in-plane in a clockwise direction. For a clockwise rotation of the proof mass 702, the capacitors 20 and 26 decrease in capacitance and the capacitors 22 and 24 increase in capacitance such as the bridge in
Under a positive z-axis magnetic field the proof mass 702 experiences a positive x-axis torque causing the proof mass 702 to rotate out-of-plane around axis 720 in a positive RX motion. This rotation causes the top of the proof mass 702 to move up and the bottom of the proof mass 702 to move down, causing the capacitor 714 to decrease and the capacitor 716 to increase.
In
The magnetized magnetic material 812 is partially disposed over the proof mass 802. The anchor 808 is connected to the substrate and the spring 804 connects the proof mass 802 to anchor 808 suspending the proof mass from the substrate. The sensing elements 20 and 22 are positioned substantially in the middle of the proof mass 802, such that they are sensitivity to y-axis motion of proof mass 802 and nominally reject RZ motion and all other motions of proof mass 802. The sensing elements 24 and 26 are positioned such that they are sensitivity to RZ motion of proof mass 802 and nominally reject y-axis and all other motions of proof mass 802.
When the MEMS device 800 undergoes external y-axis acceleration the proof mass 802 experiences a negative y-axis force and moves in the negative y direction. The y-axis motion of proof mass 802 is detected with capacitors 20 and 22, while capacitors 24 and 26 nominally remain unchanged
In the MEMS device 800, the magnetization of the magnetized magnetic materials 812 is along the positive y-axis. Under an external x-axis magnetic field the proof mas will experience a negative RZ torque causing proof mass 802 to rotate in-plane in a negative RZ direction (clockwise direction). The motion is detected with capacitors 24 and 26, while capacitors 20 and 22 nominally remain unchanged.
MEMS device 800, allows for simultaneous ambient magnetic field and ambient acceleration sensing increasing the data output rate. Here the sensing elements are driven and the output of the sensor is a single point connected to the proof mass 802 through the anchor 808. To differentiate the two signals at the single output the sensing elements are driven at different frequencies. The single output point is demodulated at two frequencies to separate the response from ambient acceleration and ambient magnetic field. Capacitors 20 and 22 are excited and demodulated at the single output point at frequency 1 to determine the ambient acceleration response and capacitors 24 and 26 are excited and demodulated at the single output point at frequency 2 to determine the response to ambient magnetic field.
In MEMS device 800 due to fabrication variations can cause the rotation center to be misaligned with the mass center. This imperfection will have the following imperfect effect. When MEMS device 800 undergoes ambient y-axis acceleration the proof mass 802 will experience a negative y-axis force and a RZ torque. Resulting in a y-axis translation and a RZ rotation. The motion will be detected with capacitors 20-26. When MEMS device 800 undergoes ambient x-axis magnetic field the proof mass 802 will experience a negative RZ torque and y axis force. Resulting in a negative RZ rotation and a y-axis motion. The motion will be detected with capacitors 20-26.
In MEMS device 800 the rotation center can be misaligned with the mass center either due to fabrication variations or intentionally designed. The method below describes how to experimentally determine this misalignment and use a signal processor to compensate for it. A signal processor uses the response from the capacitors 20-26 to extract the response from ambient acceleration and ambient magnetic field. The output of the sensor can be described by the following equation
Differential capacitance change for an RZ motion of the proof mass (δCRZ)
δCRZ=C24−C26
Differential capacitance change for a y axis motion of the proof mass (δCy)
δCY=C22−C20
To extract the response from ambient magnetic field (Mx-axis) and ambient acceleration (Ay-axis) the four quantities A, B, C and D are required from the below equation
M
x-axis
=A*δC
RZ
+B*δC
Y
A
y-axis
=C*δC
RZ
+D*δC
Y
To extract the coefficients A, B, C and D the device is excited using an electrostatic or magnetic self test shown by 820. First the device is resonated with the self-test at the rotating RZ-axis modal frequency with a known magnitude. Quantity A can be determined by measuring the response of δCRZ. Quantity B can be determined by measuring the response of δCY. Secondly the device is resonated with this self-test at the translating Y-axis modal frequency with a known magnitude. Quantity C can be determined by measuring the response of δCRZ. Quantity D can be determined by measuring the response of δCY. Once quantities A, B, C and D are known the signal processor can combined capacitors 22-26 and output the response of ambient magnetic field and ambient acceleration
The anchor 912 is rigidly connected to the substrate and is rigidly suspending the frame 930. The proof mass 902 is connected to the frame 930 by the spring 916. Proof mass 904 is connected to the frame 930 by the spring 918. The proof mass 902 is substantially 90 degrees rotated relative to the proof mass 904. Proof mass 904 has four in-plane sensing elements, 20-26, and has two out-of-plane sensing elements 922 and 924. Proof mass 902 has four in-plane sensing elements 20′-26′ and has two out-of-plane sensing elements 926 and 928.
The magnetic material 906 is disposed partially on proof mass 902 and is magnetized along the x-axis. The magnetic material 910 is disposed partially on proof mass 904 and is magnetized along the y-axis.
The proof mass 904 is unbalance about the x-axis and is heavier on the positive y-axis so that external positive z-axis acceleration causes a negative RX rotation of proof mass 904. The proof mass 902 is unbalance about the y-axis and is heavier on the negative x-axis so that external positive z-axis acceleration causes a positive RY rotation of proof mass 902.
The detection of the six inputs is done by selecting the correct combination of sensing elements.
MEMS device 1000 under a z-axis ambient acceleration response the same as MEMS device 400. MEMS device 1000 under ambient z-axis magnetic field behaves differently to MEMS device 400. Only proof mass 406 in MEMS device 1000 response to ambient magnetic field and proof mass 404 in MEMS device 1000 does not respond. The signal processor can determine the ambient z-axis acceleration response by combining the response of capacitors 24-26 or capacitors 22-26 and the ambient z-axis magnetic response is determined by combining the response of capacitors 20-26.
Although the description has been described with respect to particular embodiments thereof, these particular embodiments are merely illustrative, and not restrictive.
As used in the description herein and throughout the claims that follow, “a”, “an”, and “the” includes plural references unless the context clearly dictates otherwise. Also, as used in the description herein and throughout the claims that follow, the meaning of “in” includes “in” and “on” unless the context clearly dictates otherwise.
Thus, while particular embodiments have been described herein, latitudes of modification, various changes, and substitutions are intended in the foregoing disclosures, and it will be appreciated that in some instances some features of particular embodiments will be employed without a corresponding use of other features without departing from the scope and spirit as set forth. Therefore, many modifications may be made to adapt a particular situation or material to the essential scope and spirit.
This application claims priority to U.S. Provisional Application No. 61/794,009 filed on Mar. 15, 2013, entitled “Magnetometer Using Magnetic Material on Accelerometer”, by Seeger et al., the disclosure of which is incorporated herein by reference as though set forth in full.
Number | Date | Country | |
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61794009 | Mar 2013 | US |