Small-sized integrated navigation system

Author

Veremeenko, K.K. ; Antonov, D.A. ; Zharkov, V.M. ; Zimin, R.Yu. ; Tchernodoubov, A.Yu.

Author_Institution

Moscow Aviation Inst., State Tech. Univ., Moscow, Russia

Volume

26

Issue

3

fYear

2011

fDate

3/1/2011 12:00:00 AM

Firstpage

39

Lastpage

41

Abstract

Strap-down inertial and satellite system BISNS-1T developed by these authors from the Moscow Aviation Institute and JSC “Transas-Telematics” at the request of the Joint-Stock Company “Transas-Aviation” is presented. The main objective of this presentation is to acquaint our audience with the structure features, design, and algorithms of the system, allowing us to raise the accuracy and integrity of the navigation data and to show the results of its natural tests: at the test-bench and on a vehicle. The structure and design of the system were defined taking into account that it should be installed aboard the unmanned aerial vehicle, “Dozor” (Joint-Stock Company “Transas”).

Keywords

artificial satellites; avionics; inertial navigation; remotely operated vehicles; Transas-Aviation; satellite system; small-sized integrated navigation system; strap-down inertial system; unmanned aerial vehicle; Antenna measurements; Capacitive sensors; Magnetic separation; Measurement uncertainty; Navigation; Vibration measurement;

fLanguage

English

Journal_Title

Aerospace and Electronic Systems Magazine, IEEE

Publisher

ieee

ISSN

0885-8985

Type

jour

DOI

10.1109/MAES.2011.5746184

Filename

5746184