A study of the re-entry orbit discrepancy involving tethered satellites

Author:

Lovell T.Alan,Cochran Jr John E,Cicci David A,Cho Sungki

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. S. Cho, J.E. Cochran Jr., D.A. Cicci, Identification and orbit determination of tethered satellite systems, Journal of Applied Mathematics and Computation 117 (2001) 301–312.

2. F.R. Hoots, R.L. Roehrich, V.G. Szebehely, Space shuttle tethered satellite analysis, Technical Report #83-5, Directorate of Astrodynamics, Peterson Air Force Base, CO, August 1983.

3. T.A. Asher, D.G. Boden, R.J. Tegtmeyer, Tethered satellites: the orbit determination problem and missile early warning systems, AIAA 88-4284, presented at the AAS/AIAA Astrodynamics Conference, Minneapolis, MN, August 15–17, 1988.

4. R.A. Racca, J.J.F. Liu, J.K. Feldman, Conditions for apparent Earth-impacting orbits of tethered space objects, Technical Report #97-22, Directorate of Analysis and Engineering, Falcon Air Force Base, CO, January 1998.

5. R.A. Racca, J.K. Feldman, Eccentricity effects on apparent Earth-impacting orbits of tethered space objects, Technical Report #98-9, Directorate of Analysis and Engineering, Falcon Air Force Base, CO, April 1998.

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