System and method for providing a simple and reliable inertia measurement unit (IMU)
First Claim
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1. An inertia measurement module for an unmanned aircraft, said inertia measurement module comprising:
- a weight block assembly comprising a first weight block and a second weight block coupled together to form an inner chamber therein;
a first circuit board comprising one or more sensors, said first circuit board being supported within the inner chamber of the weight block assembly;
a housing assembly configured to support the weight block assembly therein, wherein the housing assembly is mounted onto a second circuit board located outside of said housing assembly; and
a signal line that connects the first circuit board with the second circuit board, wherein the signal line is (1) coupled to a first edge of the first circuit board and (2) extends out of openings from the weight block assembly and the housing assembly to the second circuit board, wherein said openings are located proximal to a second edge of the first circuit board that is different from the first edge of the first circuit board.
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Abstract
System and method can support a measurement module on a movable object. The measurement module includes a first circuit board with one or more sensors. Additionally, the measurement module includes a weight block assembly, wherein the weight block assembly is configured to have a mass that keeps an inherent frequency of the measurement module away from an operation frequency of the movable object. Furthermore, said first circuit board can be disposed in an inner chamber within the weight block assembly.
31 Citations
30 Claims
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1. An inertia measurement module for an unmanned aircraft, said inertia measurement module comprising:
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a weight block assembly comprising a first weight block and a second weight block coupled together to form an inner chamber therein; a first circuit board comprising one or more sensors, said first circuit board being supported within the inner chamber of the weight block assembly; a housing assembly configured to support the weight block assembly therein, wherein the housing assembly is mounted onto a second circuit board located outside of said housing assembly; and a signal line that connects the first circuit board with the second circuit board, wherein the signal line is (1) coupled to a first edge of the first circuit board and (2) extends out of openings from the weight block assembly and the housing assembly to the second circuit board, wherein said openings are located proximal to a second edge of the first circuit board that is different from the first edge of the first circuit board. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 29)
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15. A method for assembling an inertia measurement module for an unmanned aircraft, said method comprising:
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providing a first circuit board comprising one or more sensors; providing a weight block assembly that is formed by coupling a first weight block and a second weight block together to form an inner chamber therein, and supporting the first circuit board comprising the one or more sensors within the inner chamber of the weight block assembly; providing a housing assembly and supporting the weight block assembly therein, wherein the housing assembly is mounted onto a second circuit board located outside of said housing assembly; and providing a signal line that connects the first circuit board with the second circuit board, wherein the signal line is (1) coupled to a first edge of the first circuit board and (2) extends out of openings from the weight block assembly and the housing assembly to the second circuit board, wherein said openings are located proximal to a second edge of the first circuit board that is different from the first edge of the first circuit board. - View Dependent Claims (16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 30)
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Specification