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Nonlinear dynamics and reconfiguration control of two-satellite Coulomb tether formation at libration points

  • Published:2014-12 Issue: Volume:39 Page:501-512
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Huang Jing,Ma Guangfu,Liu Gang

Funder

National Natural Science Foundation of China

China Scholarship Council

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Analytical and numerical analysis of static Coulomb formations;Berryman,2005

2. Analytical charge analysis for 2- and 3-craft Coulomb formations;Berryman;AIAA J. Guidance Control Dyn.,2007

3. Deployment and retrieval of a rotating triangular tethered satellite formation near libration points;Cai;Acta Astronaut.,2014

4. Dynamical modelling and control of space tethers: a review of space tether research;Chen;Nonlinear Dyn.,2014

5. J.H. Cover, W. Knauer, H.A. Maurer, Lightweight reflecting structures utilizing electrostatic inflation, US Patent 3,546,706, Oct. 1966.

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