MATEC Web Conf.
Volume 75, 20162016 International Conference on Measurement Instrumentation and Electronics (ICMIE 2016)
|Number of page(s)||4|
|Published online||01 September 2016|
- “Designing descent unmanned spacecraft” edited by Corresponding member of the Academy of Sciences of the USSR Kovtunenko V.M. M.: “Engineering” (1985)
- V.P. Kazakoztsev, Chen Danhe, V.V. Koryanov, Method for calculation spacecraft longitudinal motion parameters during landing on the surface of a small celestial body. Herald of the Bauman Moscow State Technical University, series: Mechanical Engineering. 1 (2014) (94). p. 26–35
- V.P. Kazakovtsev, V.V. Koryanov, Chen Danhe. Dynamics of landing a spacecraft on a celestial body with small field of gravity // 2015 5th international workshop on computer science and engineering: information processing and control engineering, WCSE 2015-IPCE (Information Processing and Control Engineering, Programme (2015)) p. 191–195
- V.P. Kazakovtsev, V.V. Koryanov, Chen Danhe. Investigation of the dynamics of the angular motion of the spacecraft when landing on a celestial body with a small field of gravitation. // Flight. 10 (2014) p. 47–53
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- Zhijun Zhao, Research on the asteroid landing mechanism and its penetrating and anchoring. Dissertation for the Doctoral Degree in Engineering. Harbin Institute of Technology. (2014) p.2–25
- E. Robert Lavender. Touchdown Dynamics Analysis of Spacecraft for Soft Lunar Landing. NASA Technical Note D-2001 (1964)
- V.V. Koryanov, Method of calculating the descent of the spacecraft in the atmosphere using technology adaptation landing in different environmental conditions // Proceedings of the International Astronautical Congress, IAC 8 (2014) p.5628–5632
- V.V. Koryanov, V.P. Kazakovtsev, Method for calculating the motion parameters of spacecraft. Natural and Technical Sciences. 9-10 (77) (2014) p. 179–184
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