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A Process Method and Simulation Analysis of Spacecraft Wing Root Cable Fixing

  • Kai XuEmail author
  • Lijian Zhang
  • Hao Li
Conference paper
Part of the Lecture Notes in Electrical Engineering book series (LNEE, volume 550)

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.

Keywords

Multiple deployment of solar wing Root cable Process method Simulation analysis 

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Copyright information

© Springer Nature Singapore Pte Ltd. 2019

Authors and Affiliations

  1. 1.Beijing Institute of Spacecraft Environment EngineeringBeijingChina
  2. 2.Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace ProductBeijingChina

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