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Nonlinear control of sway in a tethered satellite system via attitude control of the main satellite

  • Published:2017-04 Issue: Volume:63 Page:317-327
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Yousefian Peyman,Salarieh Hassan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Review on dynamics and control of nonelectrodynamic tethered satellite systems;Kumar;J. Aerosp. Eng.,2006

2. Attitude control of space platform based tethered satellite system;Modi;J. Aerosp. Eng.,1998

3. Stabilization control of the tethered satellite system using nonlinear model predictive control;Liu,2014

4. Dynamic behavior of electrodynamic tether deorbit system on elliptical orbit and its control by Lorentz force;Yamaigiwa;Aerosp. Sci. Technol.,2005

5. Operational use of guided reentry capsules – system design solutions and mission safety considerations;Burkhardt;Aerosp. Sci. Technol.,2004

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