{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,10,12]],"date-time":"2025-10-12T04:18:08Z","timestamp":1760242688020,"version":"build-2065373602"},"reference-count":22,"publisher":"MDPI AG","issue":"3","license":[{"start":{"date-parts":[[2016,2,26]],"date-time":"2016-02-26T00:00:00Z","timestamp":1456444800000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0\/"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["Sensors"],"abstract":"<jats:p>The emergence of hypersonic technology pose a new challenge for inertial navigation sensors, widely used in aerospace industry. The main problems are: extremely high temperatures, vibration of the fuselage, penetrating acoustic radiation and shock N-waves. The nature of the additional errors of the gyroscopic inertial sensor with hydrostatic suspension components under operating conditions generated by forced precession of the movable part of the suspension due to diffraction phenomena in acoustic fields is explained. The cause of the disturbing moments in the form of the Coriolis inertia forces during the transition of the suspension surface into the category of impedance is revealed. The boundaries of occurrence of the features on the resonance wave match are described. The values of the \u201cfalse\u201d angular velocity as a result of the elastic-stress state of suspension in the acoustic fields are determined.<\/jats:p>","DOI":"10.3390\/s16030299","type":"journal-article","created":{"date-parts":[[2016,2,26]],"date-time":"2016-02-26T10:23:39Z","timestamp":1456482219000},"page":"299","update-policy":"https:\/\/doi.org\/10.3390\/mdpi_crossmark_policy","source":"Crossref","is-referenced-by-count":23,"title":["The Additional Error of Inertial Sensors Induced by Hypersonic Flight Conditions"],"prefix":"10.3390","volume":"16","author":[{"given":"Volodimir","family":"Karachun","sequence":"first","affiliation":[{"name":"Department of Biotechnology and Engineering, National Technical University of Ukraine \u201cKyiv Polytechnic Institute\u201d, 37, Avenue Peremogy, Kyiv 03056, Ukraine"}]},{"given":"Viktorij","family":"Mel\u2019nick","sequence":"additional","affiliation":[{"name":"Department of Biotechnology and Engineering, National Technical University of Ukraine \u201cKyiv Polytechnic Institute\u201d, 37, Avenue Peremogy, Kyiv 03056, Ukraine"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-5865-7668","authenticated-orcid":false,"given":"Igor","family":"Korobiichuk","sequence":"additional","affiliation":[{"name":"Industrial Research Institute for Automation and Measurements PIAP, Jerozolimskie 202, 02-486 Warsaw, Poland"}]},{"given":"Micha\u0142","family":"Nowicki","sequence":"additional","affiliation":[{"name":"Institute of Metrology and Biomedical Engineering, Warsaw University of Technology, Boboli 8, 02-525 Warsaw, Poland"}]},{"given":"Roman","family":"Szewczyk","sequence":"additional","affiliation":[{"name":"Institute of Metrology and Biomedical Engineering, Warsaw University of Technology, Boboli 8, 02-525 Warsaw, Poland"}]},{"given":"Svitlana","family":"Kobzar","sequence":"additional","affiliation":[{"name":"Foreign Languages Department, Zhytomyr State Technological University, Chernyakhovskogo str., 103, Zh\u0443tom\u0443r 10005, Ukraine"}]}],"member":"1968","published-online":{"date-parts":[[2016,2,26]]},"reference":[{"unstructured":"Kulyk, M.S. (2015). Suborbital and Atmospheric Hypersound Technologies, National Technical University of Ukraine \u201cKPI\u201d.","key":"ref_1"},{"unstructured":"Melnyk, V.M., Karachun, V.V., Shybetskii, V.Y., and Boyko, H.V. (2015). Float Gyroscope. (109366), Patent.","key":"ref_2"},{"unstructured":"Melnyk, V.M., Karachun, V.V., Boyko, H.V., and Shybetskii, V.Y. (2015). Float Gyroscope. (109592), Patent.","key":"ref_3"},{"unstructured":"Bordachev, D.A., Ilyushin, P.A., Kazakov, B.A., Shustov, I.E., and Volyntsev, A.A. (2015, January 25\u201327). Advanced angular rate measurement device for spacecraft. Ground test results. Proceedings of the 22nd Saint Petersburg International Conference on Integrated Navigation Systems, St. Petersburg, Russia.","key":"ref_4"},{"unstructured":"Winter, F.H. (2003). 100 Years of Flight: A Chronicle of Aerospace History, 1903-2003, American Institute of Aeronautics and Astronautics.","key":"ref_5"},{"unstructured":"Barbour, N.M. (2010). 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Technol."}],"container-title":["Sensors"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/www.mdpi.com\/1424-8220\/16\/3\/299\/pdf","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2025,10,11]],"date-time":"2025-10-11T19:19:48Z","timestamp":1760210388000},"score":1,"resource":{"primary":{"URL":"https:\/\/www.mdpi.com\/1424-8220\/16\/3\/299"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2016,2,26]]},"references-count":22,"journal-issue":{"issue":"3","published-online":{"date-parts":[[2016,3]]}},"alternative-id":["s16030299"],"URL":"https:\/\/doi.org\/10.3390\/s16030299","relation":{},"ISSN":["1424-8220"],"issn-type":[{"type":"electronic","value":"1424-8220"}],"subject":[],"published":{"date-parts":[[2016,2,26]]}}}