Robust six degree-of-freedom micromachined gyroscope with anti-phase drive scheme and method of operation of the same
First Claim
1. An apparatus with six degrees of freedom and driven in anti-phase for passive relaxation of sense mode phase matching requirements comprising:
- a first and second three degree-of-freedom (3-DOF) subsystem coupled with each other in a drive-mode and driven into anti-phase oscillation to substantially reject common-mode stimuli,where each of the first and second 3-DOF subsystems comprise two proof masses and a decoupling frame, the two proof masses in each 3-DOF subsystem being collectively arranged and configured to function as both a 1-DOF drive oscillator and 2-DOF sense oscillator,where in each of the first and second 3-DOF subsystems the 1-DOF drive oscillator and 2-DOF sense oscillator are mechanically decoupled from each other and a substrate via the decoupling frame,where the two 1-DOF drive oscillators in the first and second 3-DOF subsystems are coupled with each other to collectively function as a 2-DOF coupled system and to provide a common anti-phase drive-mode resonant frequency at which the first and second 3-DOF subsystems oscillate in opposite directions,and where the two 2-DOF sense-mode oscillators in the first and second 3-DOF subsystems each provide a flat range in frequency response where the response gain and phase are stable to provide robustness to imperfections and environmental influences, and to provide matching of sense-mode amplitude and phase of the first and second 3-DOF subsystems.
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Abstract
A method of operating an anti-phase six degree-of-freedom tuning fork gyroscope system comprises the steps of driving a first three degree-of-freedom gyroscope subsystem, and driving a second three degree-of freedom gyroscope subsystem in an anti-phase mode with the first gyroscope subsystem at an anti-phase resonant frequency. Acceleration or an angular rate of motion is sensed by the first and second three degree-of-freedom gyroscope subsystems operating in a flat frequency response range where the anti-phase resonant frequency is designed. Response gain and phase are stable and environmental and fabrication perturbations are avoided by such operation. A anti-phase six degree-of-freedom tuning fork gyroscope system which operates as described is also characterized.
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Citations
39 Claims
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1. An apparatus with six degrees of freedom and driven in anti-phase for passive relaxation of sense mode phase matching requirements comprising:
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a first and second three degree-of-freedom (3-DOF) subsystem coupled with each other in a drive-mode and driven into anti-phase oscillation to substantially reject common-mode stimuli, where each of the first and second 3-DOF subsystems comprise two proof masses and a decoupling frame, the two proof masses in each 3-DOF subsystem being collectively arranged and configured to function as both a 1-DOF drive oscillator and 2-DOF sense oscillator, where in each of the first and second 3-DOF subsystems the 1-DOF drive oscillator and 2-DOF sense oscillator are mechanically decoupled from each other and a substrate via the decoupling frame, where the two 1-DOF drive oscillators in the first and second 3-DOF subsystems are coupled with each other to collectively function as a 2-DOF coupled system and to provide a common anti-phase drive-mode resonant frequency at which the first and second 3-DOF subsystems oscillate in opposite directions, and where the two 2-DOF sense-mode oscillators in the first and second 3-DOF subsystems each provide a flat range in frequency response where the response gain and phase are stable to provide robustness to imperfections and environmental influences, and to provide matching of sense-mode amplitude and phase of the first and second 3-DOF subsystems. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. An anti-phase six degree-of-freedom tuning fork gyroscope system comprising:
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a first three degree-of-freedom gyroscope subsystem; and a second three degree-of-freedom gyroscope subsystem, where the first and second gyroscope subsystems each comprise two proof masses mechanically coupled together and mechanically restrained in each gyroscope subsystem to form a two degree-of-freedom sense mode oscillator in each gyroscope subsystem, and each of the two proof masses mechanically restrained in the first and second gyroscope subsystems to function as a one degree-of-freedom drive mode oscillator so that the four proof masses function overall as a two degree-of-freedom drive mode oscillator having two primary resonance modes, namely an in-phase and anti-phase mode; drive means for driving the two degree-of-freedom drive mode oscillator in the anti-phase mode at an anti-phase resonant frequency, and where each of the two degree-of-freedom sense mode oscillators is characterized by a flat frequency response range and where the anti-phase resonant frequency is within the flat frequency response ranges of the sense mode oscillators where response gain and phase are stable. - View Dependent Claims (9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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21. A method of operating a gyroscope with six degrees of freedom comprising:
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driving a 1-DOF drive oscillator in each of a first and second three degree-of-freedom (3-DOF) gyroscope systems, which 1-DOF drive oscillators in the first and second 3-DOF systems are coupled with each other to collectively function as a 2-DOF coupled system and to provide a common anti-phase drive-mode resonant frequency at which the first and second 3-DOF subsystems oscillate in opposite directions to substantially reject common-mode stimuli, sensing a rate of angular rotation by means of a 2-DOF sense oscillator in each of a first and second three degree-of-freedom (3-DOF) gyroscope systems, each 2-DOF sense oscillator providing a flat range in its frequency response where the response gain and phase are stable to provide robustness to imperfections and environmental influences, and to provide matching of sense-mode amplitude and phase of the first and second 3-DOF subsystems; and decoupling the 1-DOF drive oscillator and the 2-DOF sense oscillator from each other and from a substrate in each of the first and second three degree-of-freedom (3-DOF) gyroscope systems. - View Dependent Claims (22, 23, 24, 25, 26, 27)
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28. A method of operating an anti-phase six degree-of-freedom tuning fork gyroscope system comprising:
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driving a first three degree-of-freedom gyroscope subsystem; and driving a second three degree-of-freedom gyroscope subsystem in an anti-phase mode with the first three degree-of-freedom gyroscope subsystem at an anti-phase resonant frequency; and sensing motion by means of the first and second three degree-of-freedom gyroscope subsystems in a flat frequency response range where the anti-phase resonant frequency is within the flat frequency response ranges where response gain and phase are stable. - View Dependent Claims (29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39)
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Specification