DocumentCode
280735
Title
Integrated navigation system architecture
Author
Smith, S.G. ; Stokes, R.F.
Author_Institution
Air Navigation Syst. Div., R. Aerosp. Establ., Farnborough, UK
fYear
1990
fDate
33009
Firstpage
42614
Lastpage
42616
Abstract
The essence of an integrated navigation system is to combine the long-term accuracy of position fixing aids such as GPS, LORAN C, and TRN with the short-term accuracy and continuous availability of the dead-reckoning systems such as INS and Doppler radar. Modern systems use Kalman filter techniques with time-varying gains and which make extensive use of mathematical models of the system dynamics to accomplish this task. An important design feature of an integrated navigation system is the provision of `graceful degradation´, with an indication of the expected level of accuracy to the user. Several conflicting aspects which have to be considered when deciding upon a system architecture are discussed
Keywords
Kalman filters; aerospace computing; aircraft instrumentation; computerised navigation; computerised signal processing; military systems; radionavigation; Doppler radar; GPS; INS; Kalman filter; LORAN C; TRN; dead-reckoning systems; graceful degradation; integrated navigation; military systems; system architecture;
fLanguage
English
Publisher
iet
Conference_Titel
Future Military Avionic Architectures, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
191134
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