Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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The study of the dynamics of the spacecraft landing on a small celestial body at different modes of fixing

Published: 24.06.2016

Authors: Chen Danhe , Koryanov V.V.

Published in issue: #6(54)/2016

DOI: 10.18698/2308-6033-2016-6-1501

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

The article presents the results of research of space lander landing variants using clamping motor and cable. We determine parameters of their work using the fixing system of space lander under different conditions. On the basis of the results of research we offer recommendations on the optimal fixing conditions of space lander on the surface of a small celestial body.

[1] Kazakovtsev V.P., Koryanov V.V., Chen Danhe. Polet - Flyght, 2014, no. 10, pp. 47-53.
[2] Kazakovtsev V.P., Chen Danhe, Koryanov V.V. Vestnik MGTU im. N.E. Baumana. Series: Mashinostroenie - Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, 2014, no. 1 (94), pp. 26-35.
[3] Kazakovtsev V.P., Koryanov V.V. Metodika rascheta parametrov dinamiki dvizheniya kosmicheskogo spuskayemogo apparata pri zhestkoy posadke na poverkhnost’ planet [Design procedure of the parameters of space lander motion dynamics at a hard landing on the planet’s surface.]. XLIII nauchnyye chteniya pamyati K.E. Tsiolkovskogo. Tezisy dokladov [XLIII Scientific Readings in Memory of K.E. Tsiolkovsky. Abstracts]. Kaluga, 2008, pp. 121-122.
[4] Zhijun Zhao. Research on the asteroid landing mechanism and its penetrating and anchoring. Dissertation for the Doctoral Degree in Engineering, 2014, Harbin Institute of Technology, pp. 24-25.
[5] Kovtunenko V.M. Proyektirovaniye spuskayemykh avtomaticheskikh kosmicheskikh apparatov [Design of launchable unmanned spacecraft]. Moscow, Mashinostroenie Publ., 263 p.
[6] Lavender R.E. Touchdown Dynamics Analysis of Spacecraft for Soft Lunar Landing. NASA Technical Note D-2001, January 1964, pp. 8-32.
[7] Hilchenbach M., Kuechemann O., Rosenbauer H. Impact on a comet: Rosetta Lander simulations. Planetary and Space Science, 2000, 48, pp. 361-369.