Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Article

Satellite navigation and ballistic support in the problem of improving inertial navigation system accuracy

Published: 26.08.2016

Authors: Ilukhin S.N., Klishin A.N., Shvyrkina O.S.

Published in issue: #9(57)/2016

DOI: 10.18698/2308-6033-2016-9-1532

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

The article gives information on the fundamentals of inertial navigation system correction with data periodically received from the satellite navigation systems, substantiates such corrections necessity, and illustrates the main types of inertial navigation system errors. We consider the ways of using satellite navigation data to improve the spacecraft flight accuracy. The study also describes in detail the inertial navigation system algorithm and analyses its observability according to satellite navigation data. The object of the study was to obtain an optimal recursive algorithm for estimating spacecraft coordinates according to the satellite navigation system discrete data.


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