Journal of Shanghai Jiaotong University

• Aeronautics & Astronautics • Previous Articles     Next Articles

Tether Dynamic Research of Electrodynamic Tether Deorbiting System

KONG Xianren,XU Dafu,LIAO Jun,WANG Benli
  

  1. (Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China)
  • Received:2009-12-15 Revised:1900-01-01 Online:2010-11-30 Published:2010-11-30

Abstract: Considering inflecting effect, this paper presents a flexible cable model, which can be used for analyzing the dynamic behavior of the electrodynamic tether (EDT) deorbiting system. The model can describe tether inflecting and bowing under action of electrodynamic drag and gravity gradient induced force, and the influences on electro motive force and electrodynamic drag. Two mathematical simulations are employed to show the differences between the flexible cable model and the drumbell model. Vibration of the EDT system during deorbiting course is discussed. The simulation result shows that vertical response is the main vibration of EDT.

CLC Number: