Model Predictive Control with Output Feedback for a Deorbiting Electrodynamic Tether System
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
2. York University, Toronto, Ontario M3J 1P3, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G000535
Reference18 articles.
1. Space Debris and Other Threats from Outer Space
2. Terminator Tether: A Spacecraft Deorbit Device
3. Advances in dynamics and control of tethered satellite systems
4. A New Kind of Dynamic Instability in Electrodynamic Tethers
5. Dynamic Stability of Electrodynamic Tethers in Inclined Elliptical Orbits
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