Small-sized integrated navigation system

Small-sized integrated navigation system

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 audie...

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Veröffentlicht in:IEEE aerospace and electronic systems magazine 2011-03, Vol.26 (3), p.39-41
Hauptverfasser: Veremeenko, K K, Antonov, D A, Zharkov, V M, Zimin, R Yu, Tchernodoubov, A Y
Format: Magazinearticle
Sprache:eng
Schlagworte:
Antenna measurements
Capacitive sensors
Magnetic separation
Measurement uncertainty
Navigation
Vibration measurement
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Beschreibung
Zusammenfassung: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").
ISSN:0885-8985
1557-959X
DOI:10.1109/MAES.2011.5746184