Skip to main content
SpringerLink
Log in

Three-component position correctable astro-inertial navigation system with a function for determining gravitational field strength

  • Fundamental Problems in Metrology
  • Published:
Measurement Techniques Aims and scope

A model for a vector gravimetric system is presented, along with results from a numerical study of its stability and efficiency in solving gravimetric problems.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Fig. 1
Fig. 2

Similar content being viewed by others

References

  1. A. Yu. Ishlinskii, Classical Mechanics and Inertial Forces [in Russian], Nauka, Moscow (1987).

    Google Scholar 

  2. V. D. Andreev, Theory of Inertial Navigation. Correction Systems [in Russian], Nedra, Moscow (1967).

    Google Scholar 

  3. E. A. Mudretsova (ed.), Gravitational Prospecting: Geophysicist’s Handbook [in Russian], Nedra, Moscow (1981).

    Google Scholar 

  4. A. S. Devyatisilnyi, “Portable gravi-inertial system based on a three-component method of inertial navigation,” Zh. Tekhn. Fiz., 79, Iss. 12, 103–105 (2009).

    Google Scholar 

  5. A. S. Devyatisilnyi and N. A. Prudkoglyad, “Modelling an astro-inertial system with random uncertainty,” Aviakosm. Priborostr., No. 11, pp. 39–44 (2007).

  6. R. Kalman, P. Falb, and M. Arbib, Outline of Mathematical Systems Theory [Russian translation], Mir, Moscow (1971).

    Google Scholar 

  7. Yu. S. Osipov and A. V. Kryazhimskii, “Problems in dynamic inversion,” Vestnik RAN, 76, No. 7, 615–624 (2006).

    Google Scholar 

  8. A. S. Devyatisilnyi and I. B. Kryzhko, “A study of conditionality in the numerical determination of the quasistationary orbit of a satellite from earthbound observations,” Kosmich. Issled., 35, No. 1, 99–101 (1997).

    Google Scholar 

  9. A. S. Devyatisilnyi and K. A. Chislov, “Model of a gravimetric satellite-inertial navigation system integrated on the basis of an interpretation of d’Alembert’s principle,” Metrologiya, No. 11, pp. 3–11 (2010).

Download references

Author information

Authors and Affiliations

  1. Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences, Vladivostok, Russia

    A. S. Devyatisilnyi & K. A. Chislov

Authors
  1. A. S. Devyatisilnyi
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. K. A. Chislov
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to A. S. Devyatisilnyi.

Additional information

Translated from Izmeritel’naya Tekhnika, No. 2, pp. 7–9, February, 2012.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Devyatisilnyi, A.S., Chislov, K.A. Three-component position correctable astro-inertial navigation system with a function for determining gravitational field strength. Meas Tech 55, 115–118 (2012). https://doi.org/10.1007/s11018-012-9926-x

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11018-012-9926-x

Keywords

Search

Navigation