Algorithm for integrated inertial-satellite navigation systems

The integration of inertial and satellite navigation systems based on optimal linear stochastic filtration is characterized by considerable computational costs of synthesized algorithms. The proposed algorithm requires minimum computational effort and enables the efficient use of integrated navigati...

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Veröffentlicht in:	Automatic control and computer sciences 2014-11, Vol.48 (6), p.368-374
Hauptverfasser:	Shcherban’, I. V., Shcherban’, O. G.
Format:	Artikel
Sprache:	eng
Schlagworte:	Computer Science Control Structures and Microprogramming
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	The integration of inertial and satellite navigation systems based on optimal linear stochastic filtration is characterized by considerable computational costs of synthesized algorithms. The proposed algorithm requires minimum computational effort and enables the efficient use of integrated navigation systems in automotive vehicles.
ISSN:	0146-4116 1558-108X
DOI:	10.3103/S014641161406008X