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Journal of Automation and Information Sciences

Publicado 12 números por año

ISSN Imprimir: 1064-2315

ISSN En Línea: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

On Integrating Navigation Systems

Volumen 31, Edición 10, 1999, pp. 95-98
DOI: 10.1615/JAutomatInfScien.v31.i10.130
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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.

CITADO POR
  1. 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

  2. Larin V. B., Tunik A.A., On inertial navigation system error correction, International Applied Mechanics, 48, 2, 2012. Crossref

  3. Larin V. B., Tunik A. A., On Inertial-Navigation System without Angular-Rate Sensors, International Applied Mechanics, 49, 4, 2013. Crossref

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