Advertisement

Springer Nature is making SARS-CoV-2 and COVID-19 research free. View research | View latest news | Sign up for updates

Docking of spacecraft in an elliptical orbit

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

Literature Cited

  1. 1.

    K. B. Alekseev and G. G. Bebenin, Control of Aerospace Vehicles [in Russian], Mashinostroenie, Moscow (1974).

  2. 2.

    N. V. Butenin, Ya. L. Lunts, and D. R. Merkin, Course in Theoretical Mechanics [in Russian], Vol. 2, Nauka, Moscow (1971).

  3. 3.

    A. L. Lebedev and V. B. Sokolov, Rendezvous in Orbit [in Russian], Mashinostroenie, Moscow (1969).

  4. 4.

    A. I. Lur'e, Analytical Mechanics [in Russian], Fizmatgiz, Moscow (1961).

  5. 5.

    B. V. Raushenbakh and E. N. Tokar', Orientation Control of Spacecraft [in Russian], Nauka, Moscow (1974).

  6. 6.

    N. V. Roze, Rigid-Body Dynamics [in Russian], Kubuch, Alam-Ata (1932).

Download references

Additional information

Institute of Cybernetics, Academy of Sciences of the Ukrainian SSR, Kiev. Translated from Prikladnaya Mekhanika, Vol. 27, No. 10, pp. 105–112, October, 1991.

Rights and permissions

Reprints and Permissions

About this article

Cite this article

Popadinets, V.I., Burlaka, V.S., Ishchenko, A.V. et al. Docking of spacecraft in an elliptical orbit. Soviet Applied Mechanics 27, 1020–1025 (1991). https://doi.org/10.1007/BF00887513

Download citation

Keywords

  • Elliptical Orbit