This paper studies the mechanism kinematics principle of the main assemblies of the differential cushion damping system for space docking mechanism, including b all-screw differential assemblies, gear differential assemblies.
In this paper, the three-body force-element dynamic model of androgynous peripheral docking mechanism with inner guide petals is proposed.
The mathematical models of docking dynamics in the process of capture are established for two spacecrafts with inner guide petal peripheral docking mechanisms.
A partial view of Space Shuttle Atlantis' payload bay, vertical stabiliser, orbital manoeuvring system pods and docking mechanism are seen with the Earth in the background.
Natural frequency of hydraulic stewart platform using in spacecraft docking mechanism test system
