Modeling Tethered Satellite Dynamics for Identification and Orbit Determination

Author:

Cochran J. E.,Cho S.,Lovell T. A.,Cicci D. A.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference11 articles.

1. BELETSKY, V.V. and LEVIN, E.V. “Dynamics of Space Tether Systems,” Vol. 83, Advances in the Astronautical Sciences, AAS, San Diego, CA, 1993, p. 76.

2. HOOTS, F. R., ROEHRICH, R. L., and SZEBEHELY, V. G. “Space Shuttle Tethered Satellite Analysis,” Technical Report #83-5, Directorate of Astrodynamics, Peterson Air Force Base, CO, August 1983.

3. ASHER, T. A., BODEN, D. G., and TEGTMEYER, R. J. “Tethered Satellites: The Orbit Determination Problem and Missile Early Warning Systems,” AIAA 88-4284, 1988.

4. COCHRAN, J. E., Jr., CHO, S., CHENG, Y.-M., and CICCI, D. A. “Dynamics and Orbit Determination of Tethered Satellite Systems,” Paper No. AAS 96-147 presented at the AAS/ AIAA Space Flight Mechanics Meeting, Austin, TX, February 12–15, 1996.

5. CHO, S., COCHRAN, J. E., JR., and CICCI, D. A. “Identification and Orbit Determination of Tethered Satellite System,” Paper No. AAS 98–101 presented at the AAS/AIAA Space Flight Mechanics Meeting, Monterey, CA, February 9–11, 1998.

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