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
Link To Document :
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