Study of the transfer between halo orbits

Acta Astronautica

Volumn 43, Issue 9-10, 1998, Pages 493-520

  Gomez G ^a   Jorba, A ^a   Simo C ^a   Masdemont, A ^b  

^a UNIVERSITY OF BARCELONA   (Spain)

^b UNIVERSITAT POLITÈCNICA DE CATALUNYA   (Spain)

Author keywords

[No Author keywords available]

Indexed keywords

BIFURCATION (MATHEMATICS); COMPUTATIONAL METHODS; EQUATIONS OF MOTION; ORBITS; SATELLITES; SOLAR SYSTEM;

FLOQUET THEORY; HALO ORBITS; RESTRICTED THREE BODY PROBLEM;

SPACE FLIGHT;

EID: 0032203268     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(98)00177-5     Document Type: Article

References (25)

1. Díez, C., Jorba, À and Simó, C., Cel. Mech., 1991, 50, 13-30.
2. Eismont, N., Dunham, D., Sho-Chiang, J. and Farquhar, R., Lunar swingby as a tool for halo-orbit optimization in Relict-2 project, in Proc. Third Int. Symp. Spacecraft Flight Dynamics, Vol. ESA SP-326, 1991, pp. 435-439.
3. Farquhar, R. D., Muhonen, D. P., Newman, C. and Heuberger, H., The first libration point satellite. Mission overview and flight history, AAS/AIAA Astrodynamics Spec. Conf., 1979.
4. Farquhar, R.D., Muhonen, D.P. and Richardson, D.L., J. Spacecraft, 1976, 14, 170-177.
5. Gómez Llibre, G. J., Martínez, R. and Simó, C., Station Keeping of Libration Point Orbits, ESOC Contract 5648/83/D/JS(SC), Final Report, 1985.
6. Gómez, G., Jorba, À, Masdemont, J. and Simó, C., Study Refinement of Semi-Analytical Halo Orbit Theory, ESOC Contract 8625/89/D/MD(SC), Final Report, 1991.
7. Gómez, G., Jorba, À, Masdemont, J. and Simó, C., in Predictability, Stability and Chaos in N-Body Dynamical Systems, ed. A. E. Roy. Plenum Press, 1991, pp. 283-290.
8. Gómez, G., Jorba, À, Masdemont, J. and Simó, C., A Dynamical Systems Approach for the Analysis of the SOHO Mission, in Proc. Third Int. Symp. Spacecraft Flight Dynamics, Vol. ESA SP-326, 1991, pp. 449-454.
9. Gómez, G., Jorba, À, Masdemont, J. and Simó, C., Cel. Mech., 1993, 56, 541-562.
10. Goudas, C.L., Icarus, 1963, 2, 1-18.
11. Hénon, M., Astron. Astroph., 1973, 28, 415-426.
12. 1 Transfer Trajectory, MAO Working Paper No. 202, 1984.
13. Hiday, L. A. and Howell, K. C. Transfers between libration-point orbits in the elliptic restricted problem. AAS/AIAA Space Flight Mechanics Meeting, Paper AAS 92-126, Colorado 1992.
14. Howell, K.C. and Hiday-Johnston, L.A., Acta Astronautica, 1994, 32, 245-254.
15. Huber, M. C. E. et al. The History of the SOHO Mission. ESA Bulletin 86. 1996, pp. 25-35.
16. Jorba, À and Simó, C., SIAM J. of Math. Analysis, 1996, 27, 1704-1737.
17. Jorba, A. and Villanueva, J., J. of Nonlinear Science, 7 (1997) 427.
18. Lawden, D. F., Optimal Trajectories for Space Navigation, Butterworths & Co. Publishers, London, 1963.
19. Masdemont, J., Estudi i Utilització de Varietats Invariants en Problemes de Mecànica Celeste. Ph D Thesis, Universitat Politècnica de Catalunya, 1991.
20. Richardson, D.L., Celestial Mechanics, 1980, 22, 231-236.
21. Richardson, D.L., Celestial Mechanics, 1980, 22, 241-253.
22. Richardson, D.L., J. Guidance and control, 1980, 3, 543-548.
23. Rodríguez-Canabal, J. Operational Halo Orbit Maintenance Technique for SOHO. Second International Symposium on Spacecraft Flight Dynamics. ESA SP-255. 1986, pp. 71-78.
24. Wiesel, W. and Shelton, W., J. Astronomical Sci., 1983, 31, 63-76.
25. Zagouras, C.G. and Kazantzis, P.G., Astroph. Space Science, 1979, 61, 389-409.