The way of small aircraft strapdown inertial navigation system transfer alignment based on information from the carrier navigation system is considered. Optimal Kalman filter was selected as the main mathematical technique for the proposed method implementation, which showed acceptable accuracy and convergence time in the set task conditions. The main features of SINS transfer alignment algorithm and the results of its operation at complex trajectory simulation are presented.


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    Titel :

    Strapdown Inertial Navigation System Transfer Alignment: Algorithmic Features and Simulation Performance Analysis


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 63 , 4 ; 618-626


    Erscheinungsdatum :

    01.12.2020


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Multiposition alignment of strapdown inertial navigation system

    Lee, J.G. / Park, C.G. / Park, H.W. | IEEE | 1993


    Two-Position Alignment of Strapdown Inertial Navigation System

    Kim, J. / Park, H. W. / Park, C. G. et al. | British Library Online Contents | 1998


    Transfer alignment of strapdown inertial navigation systems on rolling bases

    Xinlong, W. / Liangliang, S. / Shan, M. | British Library Online Contents | 2009


    Scheme of Alignment for Strapdown Inertial Navigation Systems

    Zhang, C. Y. | British Library Online Contents | 1992