The present disclosure relates to an inertia measurement module for an unmanned aircraft, which comprises a housing assembly, a sensing assembly and a vibration damper. The vibration damper comprises a first vibration-attenuation cushion; and the sensing assembly comprises a first circuit board, a second circuit board and a flexible signal line for connecting the first circuit board and the second circuit board. An inertia sensor is fixed on the second circuit board, and the first circuit board is fixed on the housing assembly. The inertia measurement module further comprises a weight block, and the second circuit board, the weight block, the first vibration-attenuation cushion and the first circuit board are bonded together. The present disclosure greatly reduces the influence of the operational vibration frequency of the unmanned aircraft on the inertia sensor and improves the measurement stability of the inertia sensor.

An improved design for a microelectromechanical device that enables multi-axis detection but is also more robust in demanding operating conditions. The device has a balanced structure formed of two oscillating inertial masses, coupled in a way that optimally utilizes inherent stiffnesses of spring structures to increase robustness of the combined device structure.

An improved design for a microelectromechanical device that enables multi-axis detection but is also more robust in demanding operating conditions. The device has a balanced structure formed of two oscillating inertial masses, coupled in a way that optimally utilizes inherent stiffnesses of spring structures to increase robustness of the combined device structure.

Couplers for selectively coupling in-plane and out-of-plane motion between moving masses are provided herein. In particular, aspects of the present application provide for a coupler configured to couple in-plane motion between moving masses while decoupling out-of-plane motion between the moving masses. The selective couplers as described herein may be used in a device, such as a microelectromechanical systems (MEMS) inertial sensor. In some embodiments, a MEMS inertial sensor comprises a first mass configured to move in-plane, a second mass configured to move in-plane and out-of-plane, and a coupler coupling the first and second masses and comprising two levers coupled to an anchor point by respective tethers and coupled to each other by a spring.

Couplers for selectively coupling in-plane and out-of-plane motion between moving masses are provided herein. In particular, aspects of the present application provide for a coupler configured to couple in-plane motion between moving masses while decoupling out-of-plane motion between the moving masses. The selective couplers as described herein may be used in a device, such as a microelectromechanical systems (MEMS) inertial sensor. In some embodiments, a MEMS inertial sensor comprises a first mass configured to move in-plane, a second mass configured to move in-plane and out-of-plane, and a coupler coupling the first and second masses and comprising two levers coupled to an anchor point by respective tethers and coupled to each other by a spring.

An anchor member supports a frame-shaped member. A first input electrode is located outside the frame-shaped member and separate from the frame-shaped member and fixed to a substrate. A second input electrode includes an electrode portion located outside the frame-shaped member and connected to the frame-shaped member. The second input electrode is displaceable in a prescribed direction. A first reference electrode is inside the frame-shaped member and fixed to the substrate. A second reference electrode includes an electrode portion located inside of the frame-shaped member and connected to the frame-shaped member. The second reference electrode is displaceable in the prescribed direction. In the structural component, the first input electrode and the electrode portion of the second input electrode are located between the frame-shaped member and a weight member in the prescribed direction in plan view in a thickness direction defined with respect to the substrate.

An anchor member supports a frame-shaped member. A first input electrode is located outside the frame-shaped member and separate from the frame-shaped member and fixed to a substrate. A second input electrode includes an electrode portion located outside the frame-shaped member and connected to the frame-shaped member. The second input electrode is displaceable in a prescribed direction. A first reference electrode is inside the frame-shaped member and fixed to the substrate. A second reference electrode includes an electrode portion located inside of the frame-shaped member and connected to the frame-shaped member. The second reference electrode is displaceable in the prescribed direction. In the structural component, the first input electrode and the electrode portion of the second input electrode are located between the frame-shaped member and a weight member in the prescribed direction in plan view in a thickness direction defined with respect to the substrate.

A MEMS gyroscope includes an anchor point unit, a sensing unit elastically connected with the anchor point unit, and a driving unit elastically connected with the anchor point unit and the sensing unit. The anchor point unit includes four corner anchor point structures arranged at four corners of the MEMS gyroscope and four central anchor points. The sensing unit includes four first mass blocks elastically connected with the corner anchor point structures and the central anchor points to form avoiding spaces, four second mass blocks arranged within the avoiding spaces, and four decoupling mass blocks. The driving unit includes four driving pieces respectively connected with outer sides of the second mass blocks. The MEMS gyroscope realizes independent detection of angular velocities of three axes and realizes differential detection and balance of vibration moment, which immune to influence of acceleration shock and quadrature error and improves detection accuracy.

A MEMS gyroscope includes an anchor point unit, a sensing unit elastically connected with the anchor point unit, and a driving unit elastically connected with the anchor point unit and the sensing unit. The anchor point unit includes four corner anchor point structures arranged at four corners of the MEMS gyroscope and four central anchor points. The sensing unit includes four first mass blocks elastically connected with the corner anchor point structures and the central anchor points to form avoiding spaces, four second mass blocks arranged within the avoiding spaces, and four decoupling mass blocks. The driving unit includes four driving pieces respectively connected with outer sides of the second mass blocks. The MEMS gyroscope realizes independent detection of angular velocities of three axes and realizes differential detection and balance of vibration moment, which immune to influence of acceleration shock and quadrature error and improves detection accuracy.

A sensor device includes a mounting member having fixation surfaces inside, and at least one electronic component directly or indirectly fixed to the fixation surfaces of the mounting member, and the mounting member constitutes a part of a casing for housing the electronic component. Further, the fixation surfaces are perpendicular to each other.