Abstract
In order to avoid the situation that the cable is damaged during the unfolding and folding process of solar wings, a spacecraft solar wing root cable tying process is designed. Through the simulation of the root-hinge cable laying process, it is concluded that setting the appropriate reserved length and cable tie point, improving the installation flexibility of the wire harness, and the wire harness can be prevented from being stressed after the connector is plugged, thereby improving the service life of the cable. Then through the simulation of the motion of the root cable, it is concluded that the interference of the root cable is not affected during the deployment of the solar wing, and the correctness of the static simulation is verified, which provides a theoretical basis for the satellite assembly operation.
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Xu, K., Zhang, L., Li, H. (2019). A Process Method and Simulation Analysis of Spacecraft Wing Root Cable Fixing. In: Sun, S., Fu, M., Xu, L. (eds) Signal and Information Processing, Networking and Computers. ICSINC 2018. Lecture Notes in Electrical Engineering, vol 550. Springer, Singapore. https://doi.org/10.1007/978-981-13-7123-3_40
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DOI: https://doi.org/10.1007/978-981-13-7123-3_40
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