350 rub
Journal Radioengineering №8 for 2017 г.
Article in number:
Inertial navigation system calculation inaccuracy modelling for the task of the crew information support
Type of article: scientific article
UDC: 629.051
Authors:

V.V. Markelov – Post-graduate Student, ITMO University (Saint Petersburg)

E-mail: vvmarkelov@gmail.com

A.V. Gurjanov – General Director of JSC «EDB «Electroavtomatika» named after P.A.Yefimov» (Saint-Petersburg) E-mail: postmaster@elavt.spb.ru

A.V. Shukalov – Ph. D. (Eng.), First Deputy General Director, Main Designer, JSC «EDB «Electroavtomatika» named after P.A.Yefimov» (Saint-Petersburg) E-mail: aviation78@mail.ru

M.O. Kostishin – Ph. D. (Eng.), Head of Sector, JSC «EDB «Electroavtomatika» named after P.A.Yefimov» (Saint-

Petersburg)

E-mail: maksim@kostishin.com

O.O. Zharinov – Ph. D. (Eng.), Associate Professor, Saint-Petersburg State University of Aerospace Instrumentation E-mail: zharinov73@hotbox.ru

Abstract:

In this research in particular was given a prognostication option for accuracy characteristics of a non-platform inertial navigational system BINS when it functions in the autonomous mode. The values of the accuracy being prognosticated will be indicated graphically or digitally on the navigational situation board display. To analyze the proposed option the BINS inaccuracies modelling and its comparison with the prognostication results will be given shortly. The proposed option for the BINS accuracy characteristics prognostication enables to provide additional information support for the crew during the flights in the routes which require to maintain the flight trajectory very accurately.

Pages: 56-61
References
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Date of receipt: 28 июня 2017 г.