| Issue |
MATEC Web Conf.
Volume 75, 2016
2016 International Conference on Measurement Instrumentation and Electronics (ICMIE 2016)
|
|
|---|---|---|
| Article Number | 04006 | |
| Number of page(s) | 4 | |
| Section | Mechanical Automation | |
| DOI | https://doi.org/10.1051/matecconf/20167504006 | |
| Published online | 01 September 2016 | |
The study of the dynamics of the spacecraft landing on a celestial body with microgravity under different fixing conditions
Bauman Moscow State Technical University, Dynamics and flight control of motion of rockets and spacecraft Department, 105005, Moscow, Russian Federation
The features of angular motion of the spacecraft when landing on the surface of a small celestial body are studied. Different variants of the spacecraft landing using clamping engines and cable are proposed and the definition of the parameters of the landing system works using a fixing system under different conditions. Optimal conditions are recommended for securing the space lander on the surface of a small celestial body.
© The Authors, published by EDP Sciences, 2016
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