1 |
Won, C.-H., Lee, J.-S., Lee, B.-S., & Eun, J.-W. 1999, ETRI Journal, 21, 29
DOI
|
2 |
Serafin, R. A. 1982, Celestial Mechanics, 26, 383
DOI
|
3 |
Cho, C.-H., Lee, B.-S., Lee, J.-S., Kim, J.-H., & Choi, K.-H. 2002, JA&SS, 19, 197
|
4 |
Walter, H. G. 1967, AJ, 72, 994
DOI
|
5 |
Boelitz, C. A. 1995, Orbit Analysis Software Survey, Proceedings of the AAS/AIAA Astrodynamics Specialists Conference 1995, AAS 95-344
|
6 |
Hoots, F. R., & Roehrich, R. L. 1980, Models for Propagation of NORAD Element Sets- Project Space Track Report No. 3 (Peterson AFB: Aerospace Defense Command)
|
7 |
URL: http://www.orbitessera.com/html/body state vectors.html (cited March 1, 2002)
|
8 |
Escobal, P. R. 1965, Methods of Orbit Determination (New York: John Wiley & Sons)
|
9 |
Beck, E. V., & Boelitz, C. A. 1997, Orbit Analysis Software Survey 1996 Update, Proceedings of the AAS/AIAA Space Flight Mechanics Conference 1997, AAS 97-100
|
10 |
Jochim, E. F., Gill, E., Montenbruck, O., & Kirschner,M. 1996, Acta Astronautica, 39, 912
DOI
ScienceOn
|
11 |
Kelso, T. S. 1997, Satellite Times, 4, 68
|
12 |
Ernandes, K. 1994, AMSAT Journal, 17, 26
|