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Model of an Onboard Vector Gravi-Inertial Navigation System

  • FUNDAMENTAL PROBLEMS IN METROLOGY
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Measurement Techniques Aims and scope

A model of navigational data integration for determining the strength of the earth’s gravitational field is proposed and studied. The capabilities of the integrated system are illustrated by a numerical simulation.

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References

  1. A. S. Devyatisilnyi and K. A. Chislov, “Three-component position correctable astro-inertial navigation system with a function for determining gravitational field strength,” Izmer. Tekhn., No. 2, 7–9 (2012); Measur. Techn., 55, No. 2, 115–118 (2012).

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This work was supported in part by the Far Eastern Division of the Russian Foundation for Basic Research (Grant No. 11-01098501-r_vostok_a) and the Far Eastern Branch, Russian Academy of Sciences (Grant No. 12-1-0-03-005).

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Authors and Affiliations

  1. Far Eastern Federal University, Vladivostok, Russia

    A. S. Devyatisilnyi

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

    K. A. Chislov

Authors
  1. A. S. Devyatisilnyi
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  2. K. A. Chislov
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Corresponding author

Correspondence to A. S. Devyatisilnyi.

Additional information

Translated from Izmeritel’naya Tekhnika, No. 11, pp. 3–6, November, 2012.

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Devyatisilnyi, A.S., Chislov, K.A. Model of an Onboard Vector Gravi-Inertial Navigation System. Meas Tech 55, 1229–1233 (2013). https://doi.org/10.1007/s11018-013-0113-5

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  • DOI: https://doi.org/10.1007/s11018-013-0113-5

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