The study of the dynamics of the spacecraft landing on a celestial body with microgravity under different fixing conditions

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...

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Bibliographische Detailangaben
Hauptverfasser: Danhe, Chen, Koryanov, Vsevolod V.
Format: Tagungsbericht
Sprache:eng
Schlagworte:
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Zusammenfassung: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.
ISSN:2261-236X
2274-7214
2261-236X
DOI:10.1051/matecconf/20167504006