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Stability and ground experiments of a spinning triangular tethered satellite formation on a low earth orbit

  • Published:2019-09 Issue: Volume:92 Page:595-604
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Yu B.S.,Huang Z.,Geng L.L.,Jin D.P.

Funder

Natural Science Foundation of China

State Key Laboratory of Structural Analysis for Industrial Equipment

Manned Space Flight Pre-research Project

Civil Aerospace Pre-research Project of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Attitude dynamics of three-body tethered systems;Misra;Acta Astronaut.,1988

2. Tethered satellite constellations in auroral observation mission;Tan,2002

3. Dynamics of a triangular tethered satellite system on a low earth orbit;Topal,2005

4. Nonlinear Control and Synchronization of Multiple Lagrangian Systems with Application to Tethered Formation Flight Spacecraft;Chung,2007

5. Coordinated formation control strategy of the rotating hub-spoke tethered formation system;Huang;J. Aerosp. Eng.,2018

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