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This issue of the journal is an outgrowth of a special session on libration-point missions that was held at the AIAA/AAS Astrodynamics Specialist Conference in Boston, Massachusetts on August 10–12, 1998. The special session commemorated the 20th anniversary of the launch of the first libration-point spacecraft, the International Sun-Earth Explorer-3 (ISEE-3). Five of the six papers presented at this special session are contained in this volume. These five articles are augmented by two reprints of historical importance and three new publications on libration points.

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References

  1. BELBRUNO, E. “Through the Fuzzy Boundary: A New Route to the Moon,” The Planetary Report, Vol. 7, No. 3, May–June 1992, pp. 8–10.

    Google Scholar 

  2. BELBRUNO, E. “Ballistic Lunar Capture Transfers Using the Fuzzy Boundary and Solar Perturbations: A Survey,” Journal of the British Interplanetary Society, Vol. 47, No. 1, January 1994, pp. 73–80.

    MathSciNet  Google Scholar 

  3. BELBRUNO, E. A. and CARRICO, J. P. “Calculation of Weak Stability Boundary Ballistic Lunar Transfer Trajectories,” AIAA Paper 2000–4142, August 2000.

  4. GOMEZ, G., et al. “A Dynamical Systems Approach for the Analysis of the SOHO Mission,” ESA SP-326, December 1991, pp. 449–454.

  5. GOMEZ, G., et al. “Study of the Transfer from the Earth to a Halo Orbit Around the Equilibrium Point L1,” Celestial Mechanics and Dynamical Astronomy, Vol. 56, 1993, pp. 541–562.

    MATH  Google Scholar 

  6. HOWELL, K. C., et al. “Application of Dynamical Systems Theory to Trajectory Design for a Libration-Point Mission,” Journal of the Astronautical Sciences, Vol. 45, No. 2, April–June 1997, pp. 161–178.

    MathSciNet  Google Scholar 

  7. LO, M.W. and ROSS, S. D. “Low-Energy Interplanetary Transfers Using the Invariant Manifolds of L1, L2, and Halo Orbits,” Advances in the Astronautical Sciences, Vol. 99, 1998, pp. 551–561.

    Google Scholar 

  8. GUZMAN, J. J., et al. “Trajectory Design Strageties that Incorporate Invariant Manifolds and Swingby,” Advances in the Astronautical Sciences, Vol. 100. 1998, pp. 629–643.

    Google Scholar 

  9. FOLTA, D. and RICHON, K. “Libration Orbit Mission Design at L2: A MAP and NGST Perspective,” AIAA Paper 98–4469, August 1998.

  10. GOMEZ, G. and MASDEMONT, J. “Some Zero Cost Transfers Between Libration-Point Orbits,” Advances in the Astronautical Sciences, Vol. 105, 2000, pp. 1199–1216.

    Google Scholar 

  11. CROSS, C. A. “Orbits for an Extra-Terrestrial Observatory,” Journal of the British Interplanetary Society, Vol. 13, No. 4, July 1954, pp. 204–207.

    Google Scholar 

  12. KLEMPERER, W. B. and BENEDIKT, E. T. “Synodic Satellites,” Astronautics, Vol. 3, No. 10, October 1958, pp. 28–29, 64–68.

    Google Scholar 

  13. COLOMBO, G. “Sui Satelliti del Sistema Terra-luna,” Rendiconti Accademia Nazionale Dei Lincei, Series 8, Vol. 28, 1960, pp. 169–172.

    MathSciNet  Google Scholar 

  14. COLOMBO, G. “The Stabilization of an Artificial Satellite at the Inferior Conjunction Point of the Earth-Moon System,” Smithsonian Astrophysical Observatory Special Report No. 80, November 1961.

  15. PAUL, E. W. and SHAPIRO, G. “Stabilization of the Lagrangian Solutions of the Three Body Problem,” Astronautica Acta, Vol. 11, 1965, pp. 410–417.

    MathSciNet  MATH  Google Scholar 

  16. RAITHEL, W. “The Role of the Cis-Lunar Libration Point in Lunar Operations,” Proceedings of the 3rd Space Congress, Cocoa Beach, Florida, March 1966.

    Google Scholar 

  17. JAMISON, D. “Uses of the Trojan Libration Points of the Earth-Sun System,” Journal of Spacecraft and Rockets, Vol. 3, No. 4, April 1966, pp. 595–596.

    Google Scholar 

  18. FARQUHAR, R. W. “Station-Keeping in the Vicinity of Collinear Libration Points with an Application to a Lunar Communications Problem,” AAS Science and Technology Series: Space Flight Mechanics Specialist Symposium, Vol. 11, 1966, pp. 519–535.

    Google Scholar 

  19. HORNBY, H. and ALLEN, W. H. “Mission to the Libration Centers,” Astronautics & Aeronautics, Vol. 4, No. 7, July 1966, pp. 78–82.

    Google Scholar 

  20. STEG, L. “Libration-Point Satellites,” XVII International Astronautical Congress Proceedings: Astrodynamics, Guidance and Control, Madrid 1966, pp. 59–64.

    Google Scholar 

  21. FARQUHAR, R.W. “Far Libration Point of Mercury?,” Astronautics & Aeronautics, Vol. 5, No. 8, August 1967, p. 4.

    Google Scholar 

  22. FARQUHAR, R.W. “Lunar Communications with Libration-Point Satellites,” Journal of Spacecraft and Rockets, Vol. 4, No. 10, October 1967, pp. 1383–1384.

    Google Scholar 

  23. NICHOLSON, F.T. “Effect of Solar Perturbation on Motion Near the Collinear Earth-Moon Libration Points,” AIAA Journal, Vol. 5, No. 12, December 1967, pp. 2237–2241.

    MATH  Google Scholar 

  24. VONBUN, F. O. “A Hummingbird for the L2 Lunar Libration Point,” NASA TN D-4468, April 1968.

  25. FARQUHAR, R.W. “The Control and Use of Libration-Point Satellites,” Stanford University Report SUDAAR-350, July 1968. (Reprinted as NASA TR R-346, September 1970.)

  26. FARQUHAR, R.W. “Future Missions for Libration-Point Satellites,” Astronautics & Aeronautics, Vol. 7, No. 5, May 1969, pp. 52–56.

    Google Scholar 

  27. NAGATOMO, M. and MATSUO, H. “Concept of a Helio-Stationary Spacecraft,” Proceedings of the Eighth International Symposium on Space Technology and Science, Tokyo, 1969, pp. 533–538.

  28. FARQUHAR, R.W. “Limit-Cycle Analysis of a Controlled Libration-Point Satellite,” Journal of the Astronautical Sciences, Vol. 17, No. 5, March–April 1970, pp. 267–291.

    MathSciNet  Google Scholar 

  29. FARQUHAR, R.W. “The Moon’s Influence on the Location of the Sun-Earth Exterior Libration Point,” Celestial Mechanics, Vol. 2, 1970, pp. 131–133.

    MATH  Google Scholar 

  30. HEPPENHEIMER, T. A. “Optimal Controls for Out-of-Plane Motion about the Translunar Libration Point,” Journal of Spacecraft and Rockets, Vol. 7, No. 9, September 1970, pp. 1087– 1092.

    Google Scholar 

  31. KAMEL, A. A. and BREAKWELL, J. V. “Stability of Motion Near Sun-Perturbed Earth-Moon Triangular Libration Points,” Periodic Orbits, Stability and Resonances, D. Reidel Publishing Co., 1970, pp. 82–90.

  32. EULER, E. A. and YU, E. Y. “Optimal Station-Keeping at Collinear Points,” Journal of Spacecraft and Rockets, Vol. 8, No. 5, May 1971, pp. 513–516.

    Google Scholar 

  33. FARQUHAR, R. W. “Comments on Optimal Controls for Out-of-Plane Motion About the Translunar Libration Point,” Journal of Spacecraft and Rockets, Vol. 8, No. 7, June 1971, pp. 815–816.

    Google Scholar 

  34. FARQUHAR, R. W. “The Utilization of Halo Orbits in Advanced Lunar Operations,” NASA TN D-6365, July 1971.

  35. TSCHAUNER, J. “Librationzentren im Sonnengestörten Räumlichen Erde-Mond-System,” Astronautica Acta, Vol. 16, 1971, pp. 5–8.

    MATH  Google Scholar 

  36. FARQUHAR, R. W. “A Halo-Orbit Lunar Station,” Astronautics & Aeronautics, Vol. 10, No. 6, June 1972, pp. 59–63.

    Google Scholar 

  37. HEPPENHEIMER, T. A. “Out-of-Plane Motion about Libration Points: Nonlinearity and Eccentricity Effects,” Celestial Mechanics, Vol. 7, 1973, pp. 177–194.

    MATH  Google Scholar 

  38. FARQUHAR, R. W. and KAMEL, A. A. “Quasi-Periodic Orbits About the Translunar Libration Point,” Celestial Mechanics, Vol. 7, 1973, pp. 458–473.

    MATH  Google Scholar 

  39. D’AMARIO, L. A. and EDELBAUM, T. N. “Minimum Impulse Three-Body Trajectories,” AIAA Journal, Vol. 12, No. 4, April 1974, pp. 455–462.

    MATH  Google Scholar 

  40. BREAKWELL, J. V., et al. “Station-Keeping for a Translunar Communication Station,” Celestial Mechanics, Vol. 10, 1974, pp. 357–373.

    MathSciNet  Google Scholar 

  41. PU, C. L. and Edelbaum, T. N. “Four-Body Trajectory Optimization,” AIAA Journal, Vol. 13, No. 3, March 1975, pp. 333–336.

    Google Scholar 

  42. LIDOV, M. L., et al. “Semi-Analytical Method for Calculating the Motion of a Space Vehicle in the Vicinity of a Collinear Libration Point,” Cosmic Research, Vol. 14, No. 6, November– December 1976, pp. 775–785.

    Google Scholar 

  43. LIDOV, M. L. and LUKYANOV, S. S. “Statistical Estimates in the Control Problem for Motion of a Space Vehicle in the Vicinity of a Collinear Libration Point,” Cosmic Research, Vol. 14, No. 6, November–December 1976, pp. 785–797.

    Google Scholar 

  44. SCHUTZ, B. E. “Orbital Mechanics of Space Colonies at L4 and L5 of the Earth-Moon System,” AIAA Paper No. 77–33, January 1977.

  45. FARQUHAR, R. W., et al. “Mission Design for a Halo Orbiter of the Earth,” Journal of Spacecraft and Rockets, Vol. 14, No. 3, March 1977, pp. 170–177.

    Google Scholar 

  46. KRASILNIKOV, P. S. and KUNITSYN, A. L. “On the Stabilization of the Collinear Libration Points of the Restricted Circular Three-Body Problem,” Celestial Mechanics, Vol. 15, 1977, pp. 41–51.

    MathSciNet  MATH  Google Scholar 

  47. HEPPENHEIMER, T. A. “Steps Toward Space Colonization: Colony Location and Transfer Trajectories,” Journal of Spacecraft and Rockets, Vol. 15, No. 5, September–October 1978, pp. 305–312.

    Google Scholar 

  48. MARKEEV, A. P. Libration Points in Celestial Mechanics and Astrodynamics, Moscow, 1978, 312 pages, in Russian. (Available on microfiche A79-15867.)

  49. LIDOV, M. L. and RABINOVICH, V. Y. “Investigation of Families of Three-Dimensional Periodic Orbits of the Three-Body Problem,” Cosmic Research, Vol. 17, No. 3, May–June 1979.

    Google Scholar 

  50. MARKEEV, A. P. “Two-Dimensional Periodic Motion of a Satellite Relative to the Center of Mass Near a Collinear Libration Point,” Cosmic Research, Vol. 17, No. 3, May–June 1979.

    Google Scholar 

  51. DUNHAM, D. “Contingency Plans for the ISEE-3 Libration-Point Mission,” AAS Paper 79– 129, June 1979.

  52. BROUCKE, R. “Traveling Between the Lagrange Points and the Moon,” Journal of Guidance and Control, Vol. 2, No. 4, July–August 1979, pp. 257–263.

    MathSciNet  MATH  Google Scholar 

  53. BREAKWELL, J. V. and BROWN, J. V. “The ‘Halo’ Family of 3-Dimensional Periodic Orbits in the Earth-Moon Restricted 3-Body Problem,” Celestial Mechanics, Vol. 20, 1979, pp. 389– 404.

    MATH  Google Scholar 

  54. AVDEYEV, Yu. F., et al. Aspects of Spacecraft Dislocations in the Neighborhood of the Libration Points of the Earth-Moon System, Moscow, 1979, 208 pages, in Russian. (Available on microfiche A80-16590.)

  55. FARQUHAR, R.W., et al. “Trajectories and Orbital Maneuvers for the First Libration-Point Satellite,” Journal of Guidance and Control, Vol. 3, No. 6, November–December 1980, pp. 549–554.

    Google Scholar 

  56. RICHARDSON, D. L. “Halo Orbit Formulation for the ISEE-3 Mission,” Journal of Guidance and Control, Vol. 3, No. 6, November–December 1980, pp. 543–548.

    Google Scholar 

  57. RICHARDSON, D. L. “Analytic Construction of Periodic Orbits about the Collinear Points,” Celestial Mechanics, Vol. 22, 1980, pp. 241–253.

    MathSciNet  MATH  Google Scholar 

  58. LUKYANOV, S. S. “Control of a Spacecraft’s Motion in the Vicinity of a Collinear Libration Point of the Circular Three-Body Problem by Means of Light Pressure,” Cosmic Research, Vol. 19, No. 4, July–August 1981, pp. 348–357.

    Google Scholar 

  59. WIESEL, W. and SHELTON, W. “Modal Control of an Unstable Periodic Orbit,” Journal of the Astronautical Sciences, Vol. 31, No. 1, January–March 1983, pp. 63–76.

    Google Scholar 

  60. MATSUO, H., et al. “Optimization of Low Thrust Trajectories for Collinear Lagrange Point Mission,” Proceedings of the Symposium on Mechanics for Space Flight, Tokyo, 1983, pp. 87–102.

  61. HOWELL, K.C. and BREAKWELL, J. V. “Almost Rectilinear Halo Orbits,” Celestial Mechanics, Vol. 32, 1984, pp. 29–52.

    MathSciNet  MATH  Google Scholar 

  62. HOWELL, K. C. “Three-Dimensional, Periodic, ‘Halo’ Orbits,” Celestial Mechanics, Vol. 32, 1984, pp. 53–71.

    MathSciNet  MATH  Google Scholar 

  63. FARQUHAR, R. and DUNHAM, D. “Libration-Point Staging Concepts for Earth-Mars Transportation,” NASA M002, June 1986, pp. 66–77.

    Google Scholar 

  64. ELIASBERG, P. E., et al. “The Flight Maintenance in the Vicinity of a Libration Centre and the One-Impulse Transfer Trajectory to the Limited Orbit in this Region,” ESA SP-255, December 1986, pp. 55–64.

  65. SIMO, C., et al. “On the Optimal Station Keeping Control of Halo Orbits,” Acta Astronautica, Vol. 15, 1987, pp. 391–397.

    Google Scholar 

  66. DUNHAM, D. W. “Utilization of Libration-Point Orbits,” Problemi di Astronautica e di Meccanica Celeste a Ricordo del Prof. G. Colombo, Atti della Accademia delle Scienze di Torino, Suppl. al Vol. 122, 1988, pp. 239–274.

    Google Scholar 

  67. RODRIGUEZ-CANABAL, J. and HECHLER, M. “Orbital Aspects of the SOHO Mission Design,” Advances in the Astronautical Sciences, Vol. 69, 1989, pp. 347–357.

    Google Scholar 

  68. FARQUHAR, R. W. and DUNHAM, D. W. “Use of Libration-Point Orbits for Space Observatories,” Observatories in Earth Orbit and Beyond, Ed. by Y. Kondo, Kluwer Academic Publishers, 1990, pp. 391–395.

  69. PERNICKA, H. J. and HOWELL, K. C. “Sun-Earth Libration Point Trajectories that Avoid the Solar Exclusion Zone,” Journal of the Astronautical Sciences, Vol. 38, No. 3, July–September 1990, pp. 269–288.

    Google Scholar 

  70. SPONAUGLE, S. J., et al. “Optimal Cycling Between Cislunar and Cismartian Libration Points with Reusable Nuclear Electric Transfer Vehicles,” Advances in the Astronautical Sciences, Vol. 75, 1991, pp. 141–161.

    Google Scholar 

  71. FARQUHAR, R. W. “Halo-Orbit and Lunar-Swingby Missions of the 1990’s,” Acta Astronautica, Vol. 24, 1991, pp. 227–234.

    Google Scholar 

  72. EISMONT, N., et al. “Lunar Swingby as a Tool for Halo-Orbit Optimization in Relict-2 Project,” ESA SP-326, December 1991, pp. 435–439.

  73. OCAMPO, C. A. and ROSBOROUGH, G. W. “Solar Sail Trajectories Near the Sun-Earth L1 Libration Point,” Advances in the Astronautical Sciences, Vol. 76, 1991, pp. 1253–1272.

    Google Scholar 

  74. GOMEZ, G., et al. “Moon’s Influence on the Transfer from the Earth to a Halo Orbit,” Predictability, Stability, and Chaos in N-Body Dynamical Systems, Plenum Press, 1991, pp. 283–290.

  75. LIDOV, M. L., et al. “Earth-Moon-Halo Orbit Flight Paths in the Vicinity of the Earth-Sun Libration Point L2,” Cosmic Research, Vol. 30, No. 4, July–August 1992, pp. 353–369.

    Google Scholar 

  76. DUNHAM, D. W., et al. “Transfer Trajectory Design for the SOHO Libration-Point Mission,” IAF Paper-92-0066, September 1992.

  77. HOWELL, K. C. and PERNICKA, H. J. “Station Keeping Method for Libration-Point Trajectories,” Journal of Guidance, Control, and Dynamics, Vol. 16, No. 1, January–February 1993, pp.151–159.

    Google Scholar 

  78. STALOS, S., et al. “Optimum Transfer to a Large-Amplitude Halo Orbit for the Solar and Heliospheric Observatory (SOHO) Spacecraft,” Advances in the Astronautical Sciences, Vol. 84, 1993, pp. 639–650.

    Google Scholar 

  79. LIDOV, M. L., et al. “Analytical Method of Calculating Motion in a Halo Orbit and the Problem of Screening the Spacecraft from Solar Radiation in Project Relict-2,” Cosmic Research, Vol. 32, No. 1, January–February 1994, pp. 1–28.

    MathSciNet  Google Scholar 

  80. PRIETO-LLANOS, T. and GOMEZ-TIERNO, M. A. “Station Keeping at Libration Points of Natural Elongated Bodies,” Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, July– August 1994, pp. 787–794.

    Google Scholar 

  81. JONES, B. L. and BISHOP, R. H. “Rendezvous Targeting and Navigation for a Translunar Halo Orbit,” Journal of Guidance, Control, and Dynamics, Vol. 17, No. 5, September–October 1994, pp. 1109–1114.

    Google Scholar 

  82. CIELASZYK, D. and WIE, B. “New Approach to Halo Orbit Determination and Control,” Journal of Guidance, Control, and Dynamics, Vol. 19, No. 2, March–April 1996, pp. 266–273.

    MATH  Google Scholar 

  83. ROBERTS, C. E. and SHORT, R. “Injection Contingency Recovery Strategies for Halo Orbit Transfer Trajectories,” AIAA Paper 96-3600-CP, July 1996.

  84. SHARER, P. and HARRINGTON, T. “Trajectory Optimization for the ACE Halo Orbit Mission,” AIAA Paper 96-3601-CP, July 1996.

  85. DI GIAMBERARDINO, P. and MONACO, S. “On Halo Orbits Spacecraft Stabilization,” Acta Astronautica, Vol. 38, 1996, pp. 903–925.

    Google Scholar 

  86. GOMEZ, G., et al. “Station-Keeping Strategies for Translunar Libration-Point Orbits,” Advances in the Astronautical Sciences, Vol. 99, 1998, pp. 949–967.

    Google Scholar 

  87. STARCHVILLE, T. F. and MELTON, R. G. “Optimal Low-Thrust Transfers to Halo Orbits About the L2 Libration Point in the Earth-Moon System (Elliptical Problem),” Advances in the Astronautical Sciences, Vol. 99, 1998, pp. 1489–1505.

    Google Scholar 

  88. BELL, J. L., et al. “Genesis Trajectory Design,” Advances in the Astronautical Sciences, Vol. 103, 2000, pp. 1525–1537.

    Google Scholar 

  89. BECKMAN, M. and GUZMAN, J. J. “Triana Mission Design,” Advances in the Astronautical Sciences, Vol. 103, 2000, pp. 1549–1568.

    Google Scholar 

  90. WILSON, R. S., et al. “Optimization of Insertion Cost for Transfer Trajectories to Libration-Point Orbits,” Advances in the Astronautical Sciences, Vol. 103, 2000, pp. 1569–1586.

    Google Scholar 

  91. HOWELL, K. C. and GUZMAN, J. J. “Spacecraft Trajectory Design in the Context of a Coherent Restricted Four-Body Problem with Application to the MAP Mission,” IAF Paper 00-A.5.06, October 2000.

  92. FARQUHAR, R.W. “The Role of the Sun-Earth Collinear Libration Points in Future Space Exploration,” Space Times, Vol. 39, No. 6, November–December 2000, pp. 9–12.

    Google Scholar 

  93. EGOROV, V. A. “Three-Dimensional Lunar Trajectories,” NASA TT F-504, 1969. (Originally published in Moscow, 1965.)

  94. HILLER, H. “Use of the Moon’s Attraction to Accelerate a Spacecraft to Hyperbolic Flight,” Journal of the British Interplanetary Society, Vol. 22, 1969, pp. 60–74.

    Google Scholar 

  95. CAMARENA, V. “L’effet de Tremplin Lunaire,” La Recherche Aerospatiale, March–April 1970, pp. 63–68.

  96. MARCHAL, C. “Complement a L’etude de L’effet de Tremplin Lunaire,” La Recherche Aerospatiale, March–April 1971, pp. 119–121.

  97. IVASHKIN, V.V. and TYPITSYN, N. N. “Use of the Moon’s Gravitational Field to Inject a Space Vehicle into a Stationary Earth-Satellite Orbit,” Cosmic Research, Vol. 9, No. 2, March– April 1971, pp. 151–159.

    Google Scholar 

  98. PIKE, J. “Earth Escape Regions Near the Moon,” AIAA Journal, Vol. 9, No. 5, May 1971, pp. 948–950.

    Google Scholar 

  99. CORNELISSE, J. W., et al. “Orbit Design for a Geomagnetic-Tail Mission,” ESA Journal, Vol. 3, No. 1, 1979, pp. 7–34.

    Google Scholar 

  100. FARQUHAR, R. W. and DUNHAM, D. W. “A New Trajectory Concept for Exploring the Earth’s Geomagnetic Tail,” AIAA Paper 80-0112, January 1980. (Also published in the Journal of Guidance and Control, Vol. 4, No. 2, March–April 1981, pp. 192–196.)

    Google Scholar 

  101. EGOROV, V. A. “Increasing the Geocentric Energy of a Space Vehicle with the Aid of Lunar Perturbations,” Cosmic Research, Vol. 18, No. 2, March–April 1980, pp. 147–151.

    Google Scholar 

  102. ROSS, D. J. “Material Capture by Double Lunar Gravity Assist,” AIAA Paper 80-1673, August 1980.

  103. FARQUHAR, R. W. “Doubly Periodic Orbits in the Sun-Earth-Moon System” NASA CP-2152, October 1980, pp. 18–1 to 18–19.

  104. TANABE, T., et al. “Visiting Libration Points in the Earth-Moon System Using a Lunar Swingby,” Proceedings of the Thirteenth International Symposium on Space Technology and Science, Tokyo, 1982, pp. 433–438.

  105. FARQUHAR, R. “ISEE-3: A Late Entry in the Great Comet Chase,” Astronautics & Aeronautics, Vol. 21, No. 9, September 1983, pp. 50–55.

    Google Scholar 

  106. FARQUHAR, R. (editor) “Special Issue on the International Cometary Explorer Mission,” Journal of the Astronautical Sciences, Vol. 33, No. 3, July–September 1985.

    Google Scholar 

  107. FARQUHAR, R.W., et al. “Orbital Acrobatics in the Sun-Earth-Moon System,” ESA SP-255, December 1986, pp. 191–198.

  108. BENDER, D. F. “The Lunar Capture Phase of the Transfer of Asteroidal Material to Earth Orbit by Means of Gravity-Assist Trajectories,” Journal of the British Interplanetary Society, Vol. 40, No. 3, March 1987, pp. 129–132.

    Google Scholar 

  109. YOKOTA, H., et al. “MUSES-A Orbital Design,” Proceedings of the 16th ISTS, Sapporo, Japan, 1988, pp. 649–654.

    Google Scholar 

  110. LEE, T., et al. “Large Inclination Change Using Lunar-Swingby Techniques,” AIAA Paper 88-4290-CP, August 1988.

  111. MARSH, S. M. and HOWELL, K. C. “Double Lunar Swingby Trajectory Design,” AIAA Paper 88-4289-CP, August 1988.

  112. DUNHAM, D.W., et al. “Double Lunar-Swingby Trajectories for the Spacecraft of the International Solar-Terrestrial Physics Program,” Advances in the Astronautical Sciences, Vol. 69, 1989, pp. 285–301.

    Google Scholar 

  113. ENGEL, C., et al. “Launch Window Expansion and Trajectory Correction Strategies Prior to the First Lunar Swingby,” Advances in the Astronautical Sciences, Vol. 69, 1989, pp. 303–317.

    Google Scholar 

  114. UESUGI, K., et al. “Design of Double Lunar Swingby Orbits for MUSES-A and GEOTAIL,” Advances in the Astronautical Sciences, Vol. 69, 1989, pp. 319–331.

    Google Scholar 

  115. UPHOFF, C. W. “The Art and Science of Lunar Gravity Assist,” Advances in the Astronautical Sciences, Vol. 69, 1989, pp. 333–346.

    Google Scholar 

  116. STALOS, S. “Calculation of Double Lunar-Swingby Trajectories: I. Keplerian Formulation,” NASA CP-3050, 1989, pp. 367–379.

  117. STALOS, S. “Calculation of Double Lunar-Swingby Trajectories: II. Numerical Solutions in the Restricted Problem of Three Bodies,” Proceedings of the 1990 Flight Mechanics/Estimation Theory Symposium, Goddard Space Flight Center, 1990.

  118. DUNHAM, D. W., et al. “A Launch Window Study for Geotail’s Double Lunar-Swingby Trajectory,” IAF Paper 90-309, October 1990.

  119. FARQUHAR, R. W. “Halo-Orbit and Lunar-Swingby Missions of the 1990’s,” Acta Astronautica, Vol. 24, 1991, pp. 227–234.

    Google Scholar 

  120. EISMONT, N., et al. “Lunar Swingby as a Tool for Halo-Orbit Optimization in Relict-2 Project,” ESA SP-326, December 1991, pp. 435–439.

  121. LIDOV, M. L., et al. “Earth-Moon-Halo Orbit Flight Paths in the Vicinity of the Earth-Sun Libration Point L2,” Cosmic Research, Vol. 30, No. 4, July–August 1992, pp. 353–369.

    Google Scholar 

  122. SHARER, P. J., et al. “Double Lunar Swingby and Lissajous Trajectory Design,” IAF Paper 92-0065, September 1992.

  123. DUNHAM, D.W. and FARQUHAR, R. W. “Trajectory Design for a Lunar Mapping and Near-Earth Asteroid Flyby Mission,” Advances in the Astronautical Sciences, Vol. 82, 1993, pp. 605–624.

    Google Scholar 

  124. UPHOFF, C. and CROUCH, M. A. “Lunar Cycler Orbits with Alternating Semi-Monthly Transfer Windows,” Journal of the Astronautical Sciences, Vol. 41, No. 2, April–June 1993, pp. 189–205.

    Google Scholar 

  125. CARRINGTON, D., et al. “Trajectory Design for the Deep Space Program Science Experiment (DSPSE) Mission,” Advances in the Astronautical Sciences, Vol. 84, 1993, pp. 157–171.

    Google Scholar 

  126. GRAZIANI, F., et al. “Geostationary Orbits from Mid-Latitude Launch Sites via Lunar Gravity Assist,” Advances in the Astronautical Sciences, Vol. 84, 1993, pp. 561–572.

    Google Scholar 

  127. SHARER, P., et al. “Control of Libration-Point Orbits Using Lunar Gravity-Assisted Transfer,” Advances in the Astronautical Sciences, Vol. 84, 1993, pp. 651–663.

    Google Scholar 

  128. UESUGI, K. “Space Odyssey of an Angel-Summary of the Hiten’s Three Year Mission,” Advances in the Astronautical Sciences, Vol. 84, 1993, pp. 607–621.

    Google Scholar 

  129. UPHOFF, C. “Uncommon Sense in Orbit Mechanics,” Advances in the Astronautical Sciences, Vol. 84, 1993, pp. 575–590.

    Google Scholar 

  130. KAWAGUCHI, J., et al. “Planet-B’s Lunar Gravity Assist Trajectory to Mars,” Advances in the Astronautical Sciences, Vol. 85, 1993, pp. 1651–1664.

    Google Scholar 

  131. KAWAGUCHI, J., et al. “On the Operation of Lunar and Interplanetary Spacecraft at ISAS,” IAF Paper 94-Q.4.348, October 1994.

    Google Scholar 

  132. KAWAGUCHI, J., et al. “On Making Use of Lunar and Solar Gravity Assists in Lunar-A, Planet-B Missions,” Acta Astronautica, Vol. 35, 1995, pp. 633–642.

    Google Scholar 

  133. PENZO, P. A., et al. “Multiple Lunar Swingbys for Small Body and Planetary Missions,” Advances in the Astronautical Sciences, Vol. 89, 1995, pp. 317–330.

    Google Scholar 

  134. SALVATORE, J. and OCAMPO, C. “Mission Design and Orbit Operations for the First Lunar Flyby Rescue Mission,” IAF Paper 99-A.2.01, October 1999.

  135. KAWAGUCHI, J. “Lessons Learned: Lunar, Earth and Solar Gravity Assist in Nozomi Mars Spacecraft,” IAF Paper 99-A.7.08, October 1999.

  136. OCAMPO, C. “Transfers to Earth-Centered Orbits Via Lunar Gravity Assist,” IAA Paper L-0408, May 2000.

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Farquhar, R.W. Introduction. J of Astronaut Sci 49, 1–9 (2001). https://doi.org/10.1007/BF03546334

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