The invention discloses a topological structure of a multi-body variable-structure satellite, which comprises a satellite I, a satellite II, a satellite III, and a load I, a load II, a load III, a load IV, a load V, a load VI, a load VII, a load VIII and a load IX which are sequentially connected from left to right, the second load and the third load are connected through a two-degree-of-freedom joint, the third load and the fourth load are connected through a three-degree-of-freedom joint, the fourth load and the fifth load are connected through a two-degree-of-freedom joint, the fifth load and the sixth load are connected through a two-degree-of-freedom joint, and the sixth load and the seventh load are connected through a three-degree-of-freedom joint. The seventh load is connected with the eighth load through a two-degree-of-freedom joint, the eighth load is connected with the ninth load through a two-degree-of-freedom joint, the first satellite is connected with the second load, the second satellite is connected with the fifth load, the third satellite is connected with the eighth load, and relative movement between satellites can be achieved.
本发明公开了一种多体变构卫星的拓扑构型,包括卫星一、卫星二、卫星三以及从左至右依次连接的载荷一、载荷二、载荷三、载荷四、载荷五、载荷六、载荷七、载荷八和载荷九,载荷一与载荷二通过二自由度关节连接,载荷二与载荷三通过二自由度关节连接,载荷三与载荷四通过三自由度关节连接,载荷四与载荷五通过二自由度关节连接,载荷五与载荷六通过二自由度关节连接,载荷六与载荷七通过三自由度关节连接,载荷七与载荷八通过二自由度关节连接,载荷八与载荷九通过二自由度关节连接,卫星一与载荷二连接,卫星二与载荷五连接,卫星三与载荷八连接,可实现卫星间的相对运动。
Topological configuration of multi-body variable-structure satellite
一种多体变构卫星的拓扑构型
12.04.2022
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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