Libration orbit mission design at l2: A map and ngst perspective

AIAA/AAS Astrodynamics Specialist Conference and Exhibit

Volumn , Issue , 1998, Pages 1-11

  Folta, David ^a   Richon, Karen ^a  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPLICATION PROGRAMS; ASTROPHYSICS; CONSTRAINED OPTIMIZATION; DESIGN; INTERPLANETARY FLIGHT; RADIATION EFFECTS; SOFTWARE DESIGN; SPACE TELESCOPES;

COLLINEAR LIBRATION POINTS; GODDARD SPACE FLIGHT CENTER; GUIDANCE NAVIGATION AND CONTROLS; INVARIANT MANIFOLD THEORY; LIBRATION POINT MISSION; LUNAR GRAVITY ASSISTS; NEXT GENERATION SPACE TELESCOPES; SOLAR RADIATION PRESSURE;

ORBITS;

EID: 84982318602     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4469     Document Type: Conference Paper

References (13)

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2. Folta, D.C.,"Multiple Lunar Flyby Targeting for the WIND Mission", AAS/AIAA Space Flight Mechanics Meeting, Austin, TX., 1996. AIAA Paper 96-3642
3. Dunham, D.W., et al. "Transfer Trajectory Design for the SOHO Libration Point Mission", 43rd Congress of the International Astronautical Federation, Washington D.C. 1992
4. Folta, D.C., "ISEE-3 Trajectory Control Utilizing Multiple Lunar Swingbys", AIAA/AAS Astrodynamics Conference, Seattle, WA. 1984
5. Carrico, J., et al, An Interactive Tool for Design and Support of Lunar, Gravity Assist, and Libration Point Trajectories", AIAA 93-1126, AIAA/AHS/ASEE Aerospace Design Conference, CA., 1993
6. Folta, D.C., "Lunar Prospector Frozen Orbit Mission Design", AIAA-98-4288, Astrodynamics Specialist Conference, Boston, MA. 1998
7. Guzman, G. et al, "Trajectory Design Strategies That Incorporate Invariant manifolds and Swingby", AAS98- 349, International Flight Mechanics Symposium, GSFC, 1998
8. Parker T.S., and Chua, L.O., Practical Numerical Algorithms for Chaotic Systems. New York:Springer- Verlag, 1989
9. Richon, K., "An Overview of the MAP Trajectory Design", AAS 97-728, AAS/AIAA Astrodynamics Specialist Conference, Idaho, 1997
10. Gomez, G., and Jorba, A., Masdemont J., and Simo, C, "Study of the Transfer from the Earth to a Halo Orbit Around the Equilibrium Point LI", Celestial Mechanics and Dynamical Astronomy, Vol. 56, No. 4, 1993, pp. 541-562
11. Barden, B.T., and Howell, K., "Using Unstable Manifolds to Generate Transfers in the Circular Restricted Problem of Three Bodies", M.S. Thesis, Purdue University, IN.. 1994
12. Folta, D.C., Librarian Orbit Control Based on State-Space Equations, M.S. Project Report, George Washington University, 1997
13. Tene, N., et al., "Using Solar Radiation Pressure to Control L2 Orbits", AAS, International Flight Mechanics Symposium, GSFC, 1998