Design of a multi-moon orbiter

Advances in the Astronautical Sciences

Volumn 114 I, Issue , 2003, Pages 669-683

  Ross, S D ^a   Koon, W S ^a   Lo, M W ^b   Marsden, J E ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

MULTI-MOON ORBITER; SPACECRAFT ORBITS;

ALGORITHMS; BALLISTICS; MOON; OPTIMIZATION; SPACECRAFT; TRAJECTORIES;

ORBITS;

EID: 1542649467     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. Bollt, E.M. and J.D. Meiss [1995], Targeting chaotic orbits to the Moon through recurrence. Physics Letters A 204, 373-378.
2. Burris, J. and C. Arberg [2002], "Missions to Kuiper Belt Now, Europa Within the Decade Are Key to Space Discoveries," National Academy of Sciences press release, July 11, 2002. (http://www4.nas.edu/news.nsf/isbn/0309084954?OpenDocument)
3. Cowing, K. [2003], "NASA Set to Unveil 'Jupiter Tour' Mission, " January 29, 2003. (http://www.spaceref.com/news/viewnews.html?id=714)
4. Gómez, G., W.S. Koon, M.W. Lo, J.E. Marsden, J. Masdemont, and S.D. Ross [2001], Invariant manifolds, the spatial three-body problem and space mission design, Paper No. AAS 01-301, presented at AAS/AIAA Astrodynamics Specialist Conference, Quebec City, Canada, Aug. 2001.
5. Heaton, A.F., N.J. Strange, J.M. Longuski, and E.P. Bonfiglio [2002], Automated Design of the Europa Orbiter Tour, Journal of Spacecraft and Rockets 39(1), 17-22.
6. Howell, C., B. Barden and M. Lo [1997], Application of dynamical systems theory to trajectory design for a libration point mission. The Journal of the Astronautical Sciences 45(2), 161-178.
7. Karl, D.M., D.F. Bird, K. Bjorkman, T. Houlihan, R. Shackelford, and L. Tupas [1999], Microorganisms in the Accreted Ice of Lake Vostok, Antarctica. Science 286, 2144-2147.
8. Koon, W.S., M.W. Lo, J.E. Marsden and S.D. Ross [1999], Constructing a Low Energy Transfer between Jovian Moons, presented at Celestial Mechanics: an international conference on celestial mechanics, Evanston, IL, Dec. 1999. Published in Contemporary Mathematics 292 [2002], 129-145.
9. Koon, W.S., M.W. Lo, J.E. Marsden and S.D. Ross [1999], Constructing a Low Energy Transfer between Jovian Moons, presented at Celestial Mechanics: an international conference on celestial mechanics, Evanston, IL, Dec. 1999. Published in Contemporary Mathematics 292 [2002], 129-145.
10. Koon, W.S., M.W. Lo, J.E. Marsden, and S.D. Ross [2000] Heteroclinic Connections between Periodic Orbits and Resonance Transitions in Celestial Mechanics, Chaos 10(2), 427-469.
11. Koon, W.S., M.W. Lo, J.E. Marsden, and S.D. Ross [2001], Resonance and capture of Jupiter comets. Celest. Mech. Dyn. Astron. 81(1-2), 27-38.
12. Koon, W.S., M.W. Lo, J.E. Marsden, and S.D. Ross [2001a], Low energy transfer to the Moon, Celest. Mech. Dyn. Astron. 81(1-2), 63-73.
13. Ludwinski, J., M. Guman, J. Johannesen, R. Mitchell and R. Staehle [1998], The Europa Orbiter Mission Design, Paper No. 98-4.2.02, presented at the 49th International Astronautic al Congress, Melbourne, Australia, Sep. 28 - Oct. 2, 1998.
14. McFarling, U.L. [2002] "Astronomers See Pluto, Jupiter as Top Missions," Los Angeles Times, July 12, 2002.
15. Platt, J. [1998], "Jupiter's moon Callisto may hide salty ocean," NASA press release 98-192, October 21, 1998. (http://www.jpl.nasa.gov/releases/98/glcallistoocean.html)
16. Ross, S.D. [2003], Trade-Off Between Fuel and Time Optimization, presented at New Trends in Astrodynamics and Applications, College Park, MD, Jan. 2003.
17. Scheeres, D.J., M.D. Guman, and B. Villac [2001], Stability analysis of planetary satellite orbiters: Application to the Europa Orbiter. J. of Guidance, Control, and Dynamics 24(4), 778-787.
18. Schroer, C.G. and E. Ott [1997], Targeting in Hamiltonian systems that have mixed regular/chaotic phase spaces. Chaos 7(4), 512-519.
19. Schoenmaekers, J., D. Horas, and J.A. Pulido [2001] SMART-1: With Solar Electric Propulsion to the Moon, 16th International Symposium on Space Flight Dynamics, Pasadena, CA, Dec. 2001.
20. Serban, R., W.S. Koon, M.W. Lo, J.E. Marsden, L.R. Petzold, S.D. Ross and R.S. Wilson [2002], Halo orbit correction maneuvers using optimal control. Automatica 38(4), 571-583.
21. Sweetser, T., R. Maddock, J. Johannesen, J. Bell, P. Penzo, A. Wolf, S. Williams, S. Matousek, and S. Weinstein [1997] Trajectory Design for a Europa Orbiter Mission: A Plethora of Astrodynamic Challenges, Paper No. AAS 97-174, presented at AAS/AIAA Space Flight Mechanics Meeting, Huntsville, AL, Feb. 1997.
22. Webster, G. [2000], "Solar system's largest moon likely has a hidden ocean," JPL press release, December 16, 2000. (http://www.jpl.nasa.gov/releases/2000/aguganymederoundup.html)
23. Yamato, H., and D.B. Spencer [2002], Trajectory Design of Spacecraft Using Invariant Manifolds, ISTS 2002-s-16, presented at International Symposium on Space Technology and Science, Matsue, Japan, May 2002.
24. Zondervan, K.P., L.J. Wood, and T.K. Caughy [1984], Optimal Low-Thrust, Three-Burn Transfers with Large Plane Changes. The Journal of the Astronautical Sciences 32, 407-427.