Multi-axis chip-scale MEMS inertial measurement unit (IMU) based on frequency modulation

US9274136B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9274136-B2
Application numberUS-201313752044-A
CountryUS
Kind codeB2
Filing dateJan 28, 2013
Priority dateJan 28, 2013
Publication dateMar 1, 2016
Grant dateMar 1, 2016

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Abstract

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A multi-axis microelectromechanical-systems (MEMS) inertial measurement unit (IMU) is fabricated in a vacuum sealed single packaged device. An FM vibratory gyroscope and an FM resonant accelerometer both for generating FM output signals is fabricated in the silicon chip using MEMS. A signal processor is coupled to the an FM vibratory gyroscope and to the FM resonant accelerometer for receiving the FM gyroscopic output signals and the FM accelerometer output signals. The signal processor generates simultaneous and decoupled measurement of input acceleration, input rotation rate, and temperature and/or temperature distribution within the IMU, self-calibration of the biases and scale factors of the IMU and its support electronics against temperature variations and other common mode errors, and reduction of the cross axis sensitivity by reducing acceleration errors in the gyroscope and rotation errors in the accelerometer.

First claim

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We claim: 1. A multi-axis microelectromechanical-systems (MEMS) inertial measurement unit (IMU) in a vacuum sealed single packaged device comprising: a single silicon chip; an FM vibratory gyroscope for generating frequency modulated (FM) gyroscopic output signals fabricated in the silicon chip using silicon MEMS technologies as part of the vacuum sealed single packaged device; an FM resonant accelerometer for generating frequency modulated (FM) accelerometer output signals fabricated in the silicon chip using silicon MEMS technologies as part of the vacuum sealed single packaged device; and a signal processor coupled to the an FM vibratory gyroscope and to the FM resonant accelerometer for receiving the frequency modulated (FM) gyroscopic output signals and the frequency modulated (FM) accelerometer output signals, the signal processor generating simultaneous and decoupled measurement of input acceleration, input rotation rate, and temperature and/or temperature distribution within the IMU, self-calibration of the biases and scale factors of the IMU and its support electronics against temperature variations and common mode errors, and reduction of the cross axis sensitivity by reducing acceleration errors in the gyroscope and rotation errors in the accelerometer, wherein the FM resonant accelerometer comprises: a tuning fork resonator having two tines with an anti-phase and in-phase mode of vibration; and a plurality of variable gap parallel plate electrodes coupled to the two tines to produce a negative electrostatic spring, where external acceleration causes a shift of both tines with in-phase motion, which changes an effective gap in the parallel plate electrodes thereby changing the effective stiffness for each tine, where the change of stiffness induces a change of an anti-phase resonant frequency, and where the change of the anti-phase resonant frequency is an FM measure of the input acceleration. 2. The MEMS IMU of claim 1 where the FM vibratory gyroscope generates a differential FM signal including two splitting frequencies with inherent self-calibration against temperature and common mode errors, where the sum of the two splitting frequencies is proportional to the sensor temperature and the difference between the two splitting frequencies provides a measure of the input rate of rotation. 3. The MEMS IMU of claim 1 where the FM resonant accelerometer generates a differential FM signal including two splitting frequencies with inherent self-calibration against temperature and common mode errors, where the sum of the two splitting frequencies is proportional to the sensor temperature and the difference between the two splitting frequencies is a measure of the input acceleration. 4. The MEMS IMU of claim 1 where the accelerometer includes two sets of variable gap parallel plate electrodes having opposite orientations so that interchangeable operation of the two sets of parallel plate electrodes reverses the polarity of an accelerometer scale factor, enabling self-calibration of bias drift by means of a differential measurement arising from the interchangeable operation of the two sets of parallel plate electrodes. 5. The MEMS IMU of claim 1 where the two tines are momentum balanced so that the anti-phase mode of vibration generates quality factors above 1,000,000 and frequency stability below 1 ppb, enabling very good FM detection resolution and stability for the gyroscope and accelerometer. 6. The MEMS IMU of claim 1 where in-phase mode of vibration of the accelerometer is arranged and configured to have a quality factor below 1,000 by providing energy dissipation through the chip or through the use of a feedback system to provide wide bandwidth and fast response time. 7. The MEMS IMU of claim 1 where the accelerometer include two tuning forks, each of the two tuning forks having the same sensitive axis, which is the axis of the anti-phase mode vibrations, but polar opposite scale factors by reversed orientation of the negative electrostatic spring produced by the parallel plate electrodes, where simultaneous and coordinated operation of the two tuning forks yields a differential FM accelerometer in which the two output frequencies are used to detect acceleration and sensor temperature at the same time, and to eliminate the effect of temperature and common mode errors on the accelerometer output. 8. MEMS IMU of claim 1 where FM resonant accelerometer comprises: a tuning fork resonator having two tines with an anti-phase and in-phase mode of vibration of the two tines; and an electrode arrangement coupled to the tines which has a capacitance as a nonlinear function of the displacement of the tines or a mechanical spring element with non-linear dependence of stiffness versus stress. 9. A multi-axis microelectromechanical-systems (MEMS) inertial measurement unit (IMU) comprising: a silicon chip; an FM vibratory gyroscope capable of generating frequency modulated (FM) gyroscopic output signals fabricated in the silicon chip using silicon MEMS technologies; an FM resonant accelerometer capable of generating frequency modulated (FM) and amplitude modulated (AM) accelerometer output signals fabricated in the silicon chip using silicon MEMS technologies; a control system configured to switch the FM accelerometer between an FM mode of operation and an AM mode of operation; and a signal processor coupled to the an FM vibratory gyroscope and to the FM resonant accelerometer for receiving the frequency modulated (FM) gyroscopic output signals and the frequency modulated (FM) accelerometer output signals, the signal processor generating decoupled measurements of input acceleration, input rotation rate, and temperature and/or temperature distribution within the IMU, self-calibration of the biases and scale factors of the IMU and its support electronics against temperature variations and common mode errors, and reduction of the cross axis sensitivity by reducing acceleration errors in the gyroscope and rotation errors in the accelerometer.

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Classifications

  • Mountings or housings not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719 · CPC title

  • G01P21/00Primary

    Testing or calibrating of apparatus or devices covered by the preceding groups · CPC title

  • in two or more dimensions · CPC title

  • by capacitive pick-up · CPC title

  • by vibratory elements · CPC title

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What does patent US9274136B2 cover?
A multi-axis microelectromechanical-systems (MEMS) inertial measurement unit (IMU) is fabricated in a vacuum sealed single packaged device. An FM vibratory gyroscope and an FM resonant accelerometer both for generating FM output signals is fabricated in the silicon chip using MEMS. A signal processor is coupled to the an FM vibratory gyroscope and to the FM resonant accelerometer for receiving …
Who is the assignee on this patent?
Univ California
What technology area does this patent fall under?
Primary CPC classification G01P21/00. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Mar 01 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).