Numerical simulation method for landing landmark deployment for small celestial body surface landing guidance

The invention discloses a landing landmark deployment numerical simulation method for small celestial body surface landing guidance, which comprises the following steps: establishing a gravel pile small celestial body surface mechanical environment, and building a weathered layer particle bed model;...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ZENG XIANGYUAN, GUO YUFEI, WEN TONGGE
Format: Patent
Sprache:chi ; eng
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