Dynamics of a Tethered Observatory at Jupiter
Author:
Affiliation:
1. Technical University of Madrid (UPM), E-28040 Madrid, Spain
2. University of Colorado, Boulder, Colorado 80309-0429
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/10.2514/1.53383
Reference24 articles.
1. Bare wire anodes for electrodynamic tethers
2. Systems analysis of electrodynamic tethers
3. Stability and control of electrodynamic tethers for de-orbiting applications
4. satellite de-orbiting by means of electrodynamic tethers part i: general concepts and requirements
5. SATELLITE DE-ORBITING BY MEANS OF ELECTRODYNAMIC TETHERS PART II: SYSTEM CONFIGURATION AND PERFORMANCE
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2. Global dynamics of a ring-tethered three-satellite system in any plane;Nonlinear Dynamics;2023-04-12
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4. Periodic Orbits and Equilibria Near Jovian Moons Using an Electrodynamic Tether;Journal of Guidance, Control, and Dynamics;2015-01
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