Gyroscopic Gravimeter

Authors

  • E. Bezvesilnaya National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Zhytomyr Polytechnic State University
  • S. Nechay National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Zhytomyr Polytechnic State University
  • L. Chepiuk National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Zhytomyr Polytechnic State University

Keywords:

aviation gravimetric system, gyroscopic gravimeter, error

Abstract

New type gyroscopic gravimeter, which differs from known types by increase of measurement precision and speed more than in ten times at the expense of error automatic compensation employment in accordance with developed gyroscopic gravimeter state evaluation algorithms has been developed. Gravimeter has two-degree-of-freedom gyro with displaced gravity center along the natural rotation axis and angle-data transducer on the gyro inside coil axis. Torqe motor is connected to the gyro output. It is mounted on the outer gyro coil axis. It is connected with output which is one the angle-data outer con axis. Computer defines revised output signal by interference automatic compensation in accordance with received algorithms.

References

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Published

2020-02-21

How to Cite

Bezvesilnaya, E. ., Nechay, S. ., & Chepiuk, L. . (2020). Gyroscopic Gravimeter . Nauka I Studia, (2). Retrieved from http://nauka-i-studia.info/ojs/index.php/pl_ojs/article/view/110

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Статьи