Tethered satellites - The orbit determination problem and missile early warning systems
Author:
Affiliation:
1. U.S. Air Force Academy, Colorado Springs, CO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-4284
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A study of the re-entry orbit discrepancy involving tethered satellites;Acta Astronautica;2003-07
2. Application of genetic algorithms to state estimation of tethered systems;Computer Methods in Applied Mechanics and Engineering;2003-04
3. Quick-Look Identification and Orbit Determination of a Tethered Satellite;The Journal of the Astronautical Sciences;2002-09
4. Identification and orbit determination of a tethered satellite system;Applied Mathematics and Computation;2001-01
5. Modeling Tethered Satellite Dynamics for Identification and Orbit Determination;The Journal of the Astronautical Sciences;2000-03
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