Anti-acceleration Disturbance Method for Pendulum Tiltmeter

DOI

10.2991/emeit.2012.25How to use a DOI?

Keywords

pendulum tiltmeter, anti-acceleration disturbance, angular acceleration.

Abstract

With the practical application of silicon micro-machined gyro driven by rotation aircraft, it is found that the rotation aircraft’s rudder surface vibration significantly influences the performance of the gyro. In this paper, as the background of the silicon micro-machined gyro, the vibration mechanism is analyzed according to the mathematics model and dynamics. Under the influence of vibration, both of the silicon pendulum's stress form and output signal are obtained. The paper proposes a reasonable installation method to suppress the vibration. The experimental result shows that the method is effective to reduce the gyro’s output signal noise. And the result is good.

Copyright

© 2012, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Hui Zhao
AU  - Fuxue Zhang
AU  - Qingwen Yan
AU  - Xing Gao
PY  - 2012/09
DA  - 2012/09
TI  - Anti-acceleration Disturbance Method for Pendulum Tiltmeter
BT  - Proceedings of the 2nd International Conference on Electronic & Mechanical Engineering and Information Technology (EMEIT 2012)
PB  - Atlantis Press
SP  - 127
EP  - 132
SN  - 1951-6851
UR  - https://doi.org/10.2991/emeit.2012.25
DO  - 10.2991/emeit.2012.25
ID  - Zhao2012/09
ER  -