Skip to main content
SpringerLink
Log in

Determination of an Estimation of Parameters of Motion of a Spacecraft on the Stage of Its Descent on the Basis of Integration of Inertial and Optoelectronic Navigation Systems

  • Published:
Cosmic Research Aims and scope Submit manuscript

Abstract

The problem of determining an estimation of current spacecraft motion parameters on the stage of its descent is solved on the basis of readings of an optoelectronic navigation system and additional information from the self-contained inertial navigation system at the most general assumptions on the nature of motion of the object and the statistical properties of the noise of the measuring devices.

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

Similar content being viewed by others

REFERENCES

  1. Baklitskii, V.K. et al., Metody fil'tratsii signalov v korrelyatsionno-ekstremal'nykh sistemakh navigatsii (Methods of Signal Filtration in Correlationally Extremal Navigation Systems), Moscow: Radio i Svyaz', 1986.

    Google Scholar 

  2. Horn, B.K.P., Robot Vision, Cambridge, USA: MIT Press, 1986. Translated under the title Zrenie robotov, Moscow: Mir, 1989.

    Google Scholar 

  3. Aggarwal, J.K. and Nandhakumar, N., On the Computation of Motion from Sequences of Images-A Review, Proc. IEEE, 1988, vol. 76, no. 8, pp. 917-935.

    Google Scholar 

  4. Andreev, V.D., Teoriya inertsial'noi navigatsii. Avtonomnye sistemy (The Inertial Navigation Theory. Self-Contained Systems), Moscow: Nauka, 1966.

    Google Scholar 

  5. Pugachev, V.S. and Sinitsyn, I.N., Stokhasticheskie differentsial'nye sistemy (Stochastic Differential Systems), Moscow: Nauka, 1985.

    Google Scholar 

  6. Okosi, T. et al., Volokonno-opticheskie datchiki (Fiber-Optic Sensors), Leningrad: Energoatomizdat, 1990.

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. Rostov Higher Military Officer-Engineering School of the Missile Forces, Russia

    S. V. Sokolov & P. V. Dolgopoly

Authors
  1. S. V. Sokolov
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. P. V. Dolgopoly
    View author publications

    You can also search for this author in PubMed Google Scholar

Rights and permissions

Reprints and permissions

About this article

Cite this article

Sokolov, S.V., Dolgopoly, P.V. Determination of an Estimation of Parameters of Motion of a Spacecraft on the Stage of Its Descent on the Basis of Integration of Inertial and Optoelectronic Navigation Systems. Cosmic Research 39, 55–60 (2001). https://doi.org/10.1023/A:1002887828333

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1023/A:1002887828333

Keywords

Search

Navigation