Space Multi-Rigid Arm System based Space Flexible Capture Arm Model Constraints Design

摘要

1. This paper focuses on requirement of the new type of space operation devices, proposes space operation soft capture technique, to develop space soft capture concept model design, soft capture mechanism kinematics/ dynamic model construction, and mainly applies current space arm system and the obtained space experiment data to develop space soft multi-body dynamic on-orbit verification. This research results provides theory and techniques support for solving the momentum impact and disturbance problem in the process of two types of satellites capture, and provides practical data support for soft multi-body dynamic model verification, and also provides theory basis for the next generation of space soft capture arm design.