Improving an analytical gyroscope azimuth mode to compensate for the ballistic deviation of a marine gyrocompass

Authors

DOI:

https://doi.org/10.15587/1729-4061.2022.259024

Keywords:

gyrocompass, gyroscope azimuth, analytical gyroscope azimuth regime, ballistic deviance, analytical compensation of errors

Abstract

One of the main errors of the gyrocompass is ballistic deviance, which occurs when maneuvering a vessel. This is an important aspect related to solving the issue of navigational safety, which is the object of this research. As part of the study, it is proposed to improve the regime of analytical gyroscope azimuth to compensate for the ballistic deviance of marine gyrocompass, which is the subject of current scientific research.

When using the classic technique for reducing ballistic deviance (physical switching of the device to the mode of gyroscope azimuth), under certain conditions the gyrocompass after the maneuver may not return to the meridian and lose its performance. At the same time, classical algorithmic compensation by calculating ballistic deviance requires information from external devices, such as a lag and/or a GPS receiver (Global Positioning System). To compensate for ballistic deviance, this work has improved the mode of analytical gyroscope azimuth, designed to enhance the accuracy of the marine gyrocompass on the maneuver, by using a third-order filter accelerometer for filtration. This makes it possible to compensate for ballistic deviance and reduce intercardinal deviance during pitching. The current paper proposes a procedure for calculating the switching time between gyrocompass modes, which makes it possible to obtain the predefined value of ballistic deviance. As a result, the improved technique to reduce deviance demonstrates an accuracy comparable to the classical one. When using this technique, the loss by gyrocompass of the properties of selectivity relative to the meridian (indication of the course) is excluded because the device does not switch to a gyroscope azimuth mode.

The proposed observation device can be used on standard gyrocompasses without the need for reconfiguration and achieve the desired value of the residual error of deviance compensation (according to calculations, up to 0.3°)

Author Biographies

Sergiy Ivanov, National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”

PhD, Associate professor, Head of Science-Research Department

Science-Research Institute of Telecommunications

Pavlo Oliinyk, National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”

PhD, Senior Researcher

Science-Research Institute of Telecommunications

Gennadii Virchenko, National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”

Doctor of Technical Sciences, Professor

Department of Descriptive Geometry, Engineering and Computer Graphics

References

  1. Zbrutskyi, O. V., Dovhopolyi, A. S., Nesterenko, O. I., Hryhoriev, V. M. (2017). Hirokompasy dlia navihatsii ta navedennia. Kyiv: Politekhnika, 200.
  2. Sharma, P. M. (2011). Theory of Marine Gyro Compass. Bhandarkar Publications, 111.
  3. Ryzhkov, L. M., Ivanov, S. V. (2006). Shliakhy zabezpechennia funktsionuvannia korektovanoho hirokompasa yak dvorezhymnoho pryladu. V naukovo-tekhnichna konferentsiya “Pryladobuduvannia: stan i perspektyvy”. Kyiv: NTUU “KPI”, 14.
  4. Chichinadze, M. V. (2018). Marine Gyrocompasses: Development and Prospects. Giroskopiya i Navigatsiya, 26 (3), 136–142. doi: https://doi.org/10.17285/0869-7035.2018.26.3.136-142
  5. Zamorsky, A. (2020). Indirect control gyrocompass for land mobile vehicles. Bulletin of Kyiv Polytechnic Institute. Series Instrument Making, 59 (1), 5–23. doi: https://doi.org/10.20535/1970.59(1).2020.210165
  6. Jaskólski, K., Felski, A., Piskur, P. (2019). The Compass Error Comparison of an Onboard Standard Gyrocompass, Fiber-Optic Gyrocompass (FOG) and Satellite Compass. Sensors, 19 (8), 1942. doi: https://doi.org/10.3390/s19081942
  7. Uspenskyi, V., Bagmut, I., Nekrasova, M. (2018). Development of method and algorithm of dynamic gyrocompassing for high­speed systems of navigation and control of movement. Eastern-European Journal of Enterprise Technologies, 1 (9 (91)), 72–29. doi: https://doi.org/10.15587/1729-4061.2018.119735
  8. Sun, J., Xu, X., Liu, Y., Zhang, T., Li, Y., Tong, J. (2017). An Adaptive Damping Network Designed for Strapdown Fiber Optic Gyrocompass System for Ships. Sensors, 17 (3), 494. doi: https://doi.org/10.3390/s17030494
  9. Liu, Y., Yang, G., Cai, Q. (2020). A Novel Method for Determination on Switch Timing Between Damping and Non-Damping Status of Strapdown Fiber Optic Gyrocompass. IEEE Access, 8, 15870–15882. doi: https://doi.org/10.1109/access.2020.2964664
  10. Sun, F., Xia, J., Ben, Y., Zu, Y. (2015). A novel EM-Log aided gyrocompass alignment for in-motion marine SINS. Optik - International Journal for Light and Electron Optics, 126 (19), 2099–2103. doi: https://doi.org/10.1016/j.ijleo.2015.05.113
  11. Gao, S., Wei, W., Zhong, Y., Feng, Z. (2014). Rapid alignment method based on local observability analysis for strapdown inertial navigation system. Acta Astronautica, 94 (2), 790–798. doi: https://doi.org/10.1016/j.actaastro.2013.10.003
  12. Smirnov, E. L., Orekhov, A. V. (1991). O metode vychisleniya inertsionnykh deviatsiy, baziruyuschemsya na ispol'zovanii matematicheskoy modeli girokompasa. Metody i tekhnicheskie sredstva morskogo sudovozhdeniya. Moscow: Mortekhinformreklama, 30–40.
  13. Ivanov, S. V., Bezvesilnaya, O. N., Ryzhkov, L. M., Staritskiy, L. P. (2003). Corrected Gyrocompass Synthesis as a System with Changeable Structure. Symposium Gyro Technology 2003. Stuttgart, 12.0–12.8.
  14. Bereza, B. V., Mumin, O. L., Skalon, A. I. (1993). Sovremennye malogabaritnye akselerometry mayatnikovogo tipa dlya sistem inertsial'noy navigatsii i upravleniya. Giroskopiya i navigatsiya, 2, 34–38.
  15. Shaydenko, A. Ya., Lapaev, A. V. (1983). Pretsizionnye nizkochastotnye akselerometry. Dep. VINIITI No. 3168-83.

Downloads

Published

2022-06-30

How to Cite

Ivanov, S., Oliinyk, P., & Virchenko, G. (2022). Improving an analytical gyroscope azimuth mode to compensate for the ballistic deviation of a marine gyrocompass . Eastern-European Journal of Enterprise Technologies, 3(5 (117), 36–46. https://doi.org/10.15587/1729-4061.2022.259024

Issue

Vol. 3 No. 5 (117) (2022): Applied physics

Section

Applied physics

License

Copyright (c) 2022 Sergiy Ivanov, Pavlo Oliinyk, Gennadii Virchenko

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

The consolidation and conditions for the transfer of copyright (identification of authorship) is carried out in the License Agreement. In particular, the authors reserve the right to the authorship of their manuscript and transfer the first publication of this work to the journal under the terms of the Creative Commons CC BY license. At the same time, they have the right to conclude on their own additional agreements concerning the non-exclusive distribution of the work in the form in which it was published by this journal, but provided that the link to the first publication of the article in this journal is preserved.

A license agreement is a document in which the author warrants that he/she owns all copyright for the work (manuscript, article, etc.).
The authors, signing the License Agreement with TECHNOLOGY CENTER PC, have all rights to the further use of their work, provided that they link to our edition in which the work was published.
According to the terms of the License Agreement, the Publisher TECHNOLOGY CENTER PC does not take away your copyrights and receives permission from the authors to use and dissemination of the publication through the world's scientific resources (own electronic resources, scientometric databases, repositories, libraries, etc.).
In the absence of a signed License Agreement or in the absence of this agreement of identifiers allowing to identify the identity of the author, the editors have no right to work with the manuscript.
It is important to remember that there is another type of agreement between authors and publishers – when copyright is transferred from the authors to the publisher. In this case, the authors lose ownership of their work and may not use it in any way.