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Model of gravimetric satellite-inertial navigation system integrated on the basis of an interpretation of the D’alembert principle

  • Fundamental Problems in Metrology
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Measurement Techniques Aims and scope

A mechanics-theoretic evaluation of the two-component method of inertial navigation is given and results of a numerical investigation of a model of a gravitational inertial navigation system constructed on the basis of this evaluation are presented.

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Authors and Affiliations

  1. Institute of Automation and Control Processes, Far Eastern Branch, Russian Academy of Sciences (IAPU DVO RAN), Vladivostok, Russia

    A. S. Devyatisilnyi & K. A. Chislov

Authors
  1. A. S. Devyatisilnyi
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  2. K. A. Chislov
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Correspondence to A. S. Devyatisilnyi.

Additional information

Translated from Metrologiya, No. 11, pp. 3–11, November, 2010.

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Devyatisilnyi, A.S., Chislov, K.A. Model of gravimetric satellite-inertial navigation system integrated on the basis of an interpretation of the D’alembert principle. Meas Tech 53, 1316–1321 (2011). https://doi.org/10.1007/s11018-011-9659-2

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  • DOI: https://doi.org/10.1007/s11018-011-9659-2

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