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Error of a Non-driven Micromechanical Gyroscope

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Abstract

The 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.

Keywords

Micromechanical Gyroscope Vibratory Gyroscope Absolute Angular Velocity Pickup Angle Output Axis 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Copyright information

© National Defense Industry Press and Springer-Verlag GmbH Germany 2018

Authors and Affiliations

  1. 1.Beijing Information Science and Technology UniversityBeijingChina
  2. 2.Academy of Armored Forces EngineeringBeijingChina

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