Исследование динамики посадки космического аппарата на малое небесное тело при разных режимах закрепления

9 / 9

Исследование динамики посадки космического аппарата на малое небесное тело…
Инженерный журнал: наука и инновации # 62016 9
The study of the dynamics of the spacecraft landing
on a small celestial body at different modes of fixing
© Danhe Chen, V.V. Koryanov
Bauman Moscow State Technical University, Moscow, 105005, Russia
The article presents the results of research of space lander landing variants using clamp-
ing 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.
Key words: space lander, small celestial body, fixing, optimal conditions.
REFERENCES
[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., Kuèchemann O., Rosenbauer H. Impact on a comet: Rosetta
Lander simulations. Planetary and Space Science, 2000, 48, рp. 361–369.
Chen Danhe, a postgraduate student of the Department of Dynamics and Control of
Rocket and Spacecraft Flight at Bauman Moscow State Technical University. Field of re-
search interests includes ballistics modelling and dynamics of spacecraft and descent ve-
hicle motion. e-mail:
Koryanov V.V. (b. 1982) graduated from Bauman Moscow State Technical University in
2006. Cand. Sci. (Eng.), Assoc. Professor of the Department of Dynamics and Control of
Rocket and Spacecraft Flight at Bauman Moscow State Technical University. Author of
more than 20 works in the field of ballistics modelling and dynamics of spacecraft and
descent vehicle motion. e-mail: