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公开(公告)号:US20190186950A1
公开(公告)日:2019-06-20
申请号:US16221409
申请日:2018-12-14
Applicant: INVENSENSE, INC.
Inventor: Sriraman Dakshinamurthy , Doruk Senkal , Ali Shirvani , Ronak Chetan Desai , Carlo Pinna
CPC classification number: G01C25/005 , B81B3/0018 , B81B7/02 , B81B2201/0242
Abstract: Microelectromechanical systems (MEMS) gyroscopes and related measurement and calibration techniques are described. Various embodiments facilitate phase estimation of an ideal phase for a demodulator mixer associated with an exemplary MEMS gyroscope using quadrature tuning, which can improve offset performance over life time for exemplary MEMS gyroscopes. Exemplary embodiments can comprise adjusting a quadrature component of an exemplary MEMS gyroscope sense signal, measuring a change in offset of the exemplary MEMS gyroscope at an output of a demodulator mixer associated with the exemplary MEMS gyroscope, estimating a phase error between the quadrature component and a demodulation phase angle of the demodulator mixer based on the change in the offset, and periodically adjusting the demodulation phase angle of the demodulator mixer based on the phase error.
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公开(公告)号:US20230324176A1
公开(公告)日:2023-10-12
申请号:US18333821
申请日:2023-06-13
Applicant: INVENSENSE, INC.
Inventor: Doruk Senkal , Robert Hennessy , Houri Johari-Galle , Joseph Seeger
IPC: G01C19/5712 , G01C19/5747 , G01C19/5762
CPC classification number: G01C19/5712 , G01C19/5747 , G01C19/5762
Abstract: A dynamically balanced 3-axis gyroscope architecture is provided. Various embodiments described herein can facilitate providing linear and angular momentum balanced 3-axis gyroscope architectures for better offset stability, vibration rejection, and lower part-to-part coupling.
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公开(公告)号:US10794702B2
公开(公告)日:2020-10-06
申请号:US16130695
申请日:2018-09-13
Applicant: INVENSENSE, INC.
Inventor: Doruk Senkal , Houri Johari-Galle , Joseph Seeger
IPC: G01C19/5712 , G01C19/5776 , G01C19/5726 , G01C25/00
Abstract: A MEMS gyroscope includes a proof mass of a suspended spring mass system that is driven at a drive frequency. The proof mass moves relative to a sense electrode such that an overlap of the proof mass and sense electrode changes during the drive motion. A Coriolis force causes the proof mass to move relative to the sense electrode. The overlap and the movement due to the Coriolis force are sensed, and angular velocity is determined based on the magnitude of a signal generated due to a change in overlap and the Coriolis force.
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公开(公告)号:US11841228B2
公开(公告)日:2023-12-12
申请号:US17467145
申请日:2021-09-03
Applicant: INVENSENSE, INC.
Inventor: Doruk Senkal , Robert Hennessy , Houri Johari-Galle , Joe Seeger
IPC: G01C19/5712 , G01C19/5783
CPC classification number: G01C19/5712 , G01C19/5783
Abstract: The subject disclosure provides exemplary 3-axis (e.g., GX, GY, and GZ) linear and angular momentum balanced vibratory rate gyroscope architectures with fully-coupled sense modes. Embodiments can employ balanced drive and/or balanced sense components to reduce induced vibrations and/or part to part coupling. Embodiments can comprise two inner frame gyroscopes for GY sense mode and an outer frame or saddle gyroscope for GX sense mode and drive system coupling, drive shuttles coupled to the two inner frame gyroscopes or outer frame gyroscope, and four GZ proof masses coupled to the inner frame gyroscopes for GZ sense mode. Components can be removed from an exemplary overall architecture to fabricate a single axis or two axis gyroscope and/or can be configured such that a number of proof-masses can be reduced in half from an exemplary overall architecture to fabricate a half-gyroscope. Other embodiments can employ a stress isolation frame to reduce package induced stress.
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公开(公告)号:US11650078B2
公开(公告)日:2023-05-16
申请号:US17825856
申请日:2022-05-26
Applicant: InvenSense, Inc.
Inventor: Doruk Senkal , Houri Johari-Galle , Joseph Seeger
IPC: G01C25/00 , G01C19/5776 , G01C19/5719 , G01C19/5726 , G01R29/02 , G01R19/00 , G01R23/00 , G01R25/00
CPC classification number: G01C25/005 , G01C19/5719 , G01C19/5726 , G01C19/5776 , G01R19/0038 , G01R23/005 , G01R25/00 , G01R29/02 , B81B2201/0242 , B81B2207/03
Abstract: A MEMS device may output a signal during operation that may include an in-phase component and a quadrature component. An external signal having a phase that corresponds to the quadrature component may be applied to the MEMS device, such that the MEMS device outputs a signal having a modified in-phase component and a modified quadrature component. A phase error for the MEMS device may be determined based on the modified in-phase component and the modified quadrature component.
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公开(公告)号:US20210396519A1
公开(公告)日:2021-12-23
申请号:US17467145
申请日:2021-09-03
Applicant: INVENSENSE, INC.
Inventor: Doruk Senkal , Robert Hennessy , Houri Johari-Galle , Joe Seeger
IPC: G01C19/5712 , G01C19/5783
Abstract: The subject disclosure provides exemplary 3-axis (e.g., GX, GY, and GZ) linear and angular momentum balanced vibratory rate gyroscope architectures with fully-coupled sense modes. Embodiments can employ balanced drive and/or balanced sense components to reduce induced vibrations and/or part to part coupling. Embodiments can comprise two inner frame gyroscopes for GY sense mode and an outer frame or saddle gyroscope for GX sense mode and drive system coupling, drive shuttles coupled to the two inner frame gyroscopes or outer frame gyroscope, and four GZ proof masses coupled to the inner frame gyroscopes for GZ sense mode. Components can be removed from an exemplary overall architecture to fabricate a single axis or two axis gyroscope and/or can be configured such that a number of proof-masses can be reduced in half from an exemplary overall architecture to fabricate a half-gyroscope. Other embodiments can employ a stress isolation frame to reduce package induced stress.
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公开(公告)号:US10996075B2
公开(公告)日:2021-05-04
申请号:US16221409
申请日:2018-12-14
Applicant: INVENSENSE, INC.
Inventor: Sriraman Dakshinamurthy , Doruk Senkal , Ali Shirvani , Ronak Chetan Desai , Carlo Pinna
Abstract: Microelectromechanical systems (MEMS) gyroscopes and related measurement and calibration techniques are described. Various embodiments facilitate phase estimation of an ideal phase for a demodulator mixer associated with an exemplary MEMS gyroscope using quadrature tuning, which can improve offset performance over life time for exemplary MEMS gyroscopes. Exemplary embodiments can comprise adjusting a quadrature component of an exemplary MEMS gyroscope sense signal, measuring a change in offset of the exemplary MEMS gyroscope at an output of a demodulator mixer associated with the exemplary MEMS gyroscope, estimating a phase error between the quadrature component and a demodulation phase angle of the demodulator mixer based on the change in the offset, and periodically adjusting the demodulation phase angle of the demodulator mixer based on the phase error.
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公开(公告)号:US20210116244A1
公开(公告)日:2021-04-22
申请号:US17138392
申请日:2020-12-30
Applicant: INVENSENSE, INC.
Inventor: Doruk Senkal , Robert Hennessy , Houri Johari-Galle , Joseph Seeger
IPC: G01C19/5712 , G01C19/5747 , G01C19/5762
Abstract: In a first aspect, the angular rate sensor comprises a substrate and a rotating structure anchored to the substrate. The angular rate sensor also includes a drive mass anchored to the substrate and an element coupling the drive mass and the rotating structure. The angular rate sensor further includes an actuator for driving the drive mass into oscillation along a first axis in plane to the substrate and for driving the rotating structure into rotational oscillation around a second axis normal to the substrate; a first transducer to sense the motion of the rotating structure in response to a Coriolis force in a sense mode; and a second transducer to sense the motion of the sensor during a drive mode. In a second aspect the angular rate sensor comprises a substrate and two shear masses which are parallel to the substrate and anchored to the substrate via flexible elements. In further embodiments, a dynamically balanced 3-axis gyroscope architecture is provided. Various embodiments described herein can facilitate providing linear and angular momentum balanced 3-axis gyroscope architectures for better offset stability, vibration rejection, and lower part-to-part coupling.
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公开(公告)号:US10746565B2
公开(公告)日:2020-08-18
申请号:US16370664
申请日:2019-03-29
Applicant: InvenSense, Inc.
Inventor: Doruk Senkal , Joseph Seeger
IPC: G01C25/00 , G01C19/5614 , G01C19/5726 , G01C19/5649 , G01C19/5776
Abstract: A method includes receiving a signal from a sensor. The signal includes a first in-phase component and a first quadrature component. The first in-phase and quadrature components are identified. A rate signal is applied to the sensor and the sensor generates a sensed rate signal. A second in-phase and quadrature components associated with the sensed rate signal are determined. A phase error based on the first and the second in-phase components, and the first and the second quadrature components is determined. The method may further include reducing error in measurements associated with the sensor by dynamically compensating for the determined phase error, e.g., by modifying a clock signal, by changing a demodulation phase of a demodulator used to identify the in-phase and the quadrature components.
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公开(公告)号:US20250164247A1
公开(公告)日:2025-05-22
申请号:US19030857
申请日:2025-01-17
Applicant: INVENSENSE, INC.
Inventor: Doruk Senkal , Robert Hennessy , Houri Johari-Galle , Joseph Seeger
IPC: G01C19/5712 , G01C19/5747 , G01C19/5762
Abstract: A dynamically balanced 3-axis gyroscope architecture is provided. Various embodiments described herein can facilitate providing linear and angular momentum balanced 3-axis gyroscope architectures for better offset stability, vibration rejection, and lower part-to-part coupling. In addition, exemplary gyroscope architectures could yield more compact but non-balanced drive and sense gyroscopes with fewer than 3 axes by omitting components of exemplary gyroscope architectures.
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