Publicado 12 números por año
ISSN Imprimir: 1064-2315
ISSN En Línea: 2163-9337
Indexed in
On Integrating Navigation Systems
SINOPSIS
Problem of correction of errors of strapdown inertial navigating system by results of estimations, which received from satellite navigating system is considered. The problem is considered within the framework of the Kalman filter. This way, algorithm of calculation of Cholesky factor of a covariance matrix is offered.
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Larin Vladimir, Tunik Anatoly, Gyro-free accelerometer-based SINS: Algorithms and structures, 2012 2nd International Conference "Methods and Systems of Navigation and Motion Control" (MSNMC), 2012. Crossref
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Larin V. B., Tunik A.A., On inertial navigation system error correction, International Applied Mechanics, 48, 2, 2012. Crossref
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Larin V. B., Tunik A. A., On Inertial-Navigation System without Angular-Rate Sensors, International Applied Mechanics, 49, 4, 2013. Crossref