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Titlebook: Non-driven Micromechanical Gyroscopes and Their Applications; Fuxue Zhang,Wei Zhang,Guosheng Wang Book 2018 National Defense Industry Pres

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11#
發(fā)表于 2025-3-23 12:07:52 | 只看該作者
Error of a Non-driven Micromechanical GyroscopeThe vibratory gyroscope is a sensor which is designed to measure the absolute angular velocity of a non-rotating aircraft, and comprises a platform which is suspended in a frame by two elastic axes (internal and external), an electrostatic actuator and an angular pickup capacitor with two axes.
12#
發(fā)表于 2025-3-23 16:42:12 | 只看該作者
Phase Shift of a Non-driven Micromechanical GyroscopeSet the following coordinate systems: ., . and . is the inertial coordinate system; ., . and . is the coordinate system of a silicon pendulum; and ., . and . is the frame coordinate system.
13#
發(fā)表于 2025-3-23 18:35:49 | 只看該作者
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發(fā)表于 2025-3-24 00:14:26 | 只看該作者
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發(fā)表于 2025-3-24 05:58:45 | 只看該作者
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16#
發(fā)表于 2025-3-24 09:13:21 | 只看該作者
17#
發(fā)表于 2025-3-24 13:48:17 | 只看該作者
Precision of a Non-driven Mechanical Gyroscope with Negative Velocity Feedbackity rotating around the horizontal axis of the aircraft is ultimately attributed to the stability of the calibration scale factor of the instrument. In this chapter, the precision of the gyroscope is studied based on the dynamic characteristics of the instrument.
18#
發(fā)表于 2025-3-24 16:06:04 | 只看該作者
Signal ProcessingTherefore the structure of a non-driven silicon micromechanical gyroscope is simple. However, the rolling angular velocity of the rotating flight carrier changes and the angular velocity is not stable such that the output stability of the micromechanical gyroscope is affected.
19#
發(fā)表于 2025-3-24 20:42:57 | 只看該作者
Fuxue Zhang,Wei Zhang,Guosheng WangSummarizes the latest studies on the micromechanical gyroscope with no driven structure.Discusses both theoretical and practical aspects of gyroscopes that can only be used on a spinning carrier.Descr
20#
發(fā)表于 2025-3-25 02:26:52 | 只看該作者
Book 2018d non-driven micromechanical gyroscopes...The book is divided into three parts, the first of which mainly addresses mathematic models, precision, performance and operating error in non-driven mechanical gyroscopes. The second part focuses on the operating theory, error, phase shift and performance e
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