References
- Beckman M, Concha M, Lunar Prospector orbit determination results, in Astrodynamics Specialist Conference, Boston, MA, 10-12 August 1998, AIAA-98-4561. http://dx.doi.org/10.2514/6.1998-4561
- Budnik F, Morley TA, MacKenzie RA, ESOC's system for interplanetary orbit determination: implementation and operational experience, in 18th International Symposium on Space Flight Dynamics, Munich, Germany, 11-15 October 2004.
- Cho DH, Jeong BY, Lee DH, Bang HC, Optimal perilune altitude of lunar landing trajectory, IJASS, 10, 67-74 (2009). http://dx.doi.org/10.5139/IJASS.2009.10.1.067
- Choi SJ, Song YJ, Bae J, Kim E, Ju G, Design and Analysis of Korean Lunar Orbiter Mission using Direct Transfer Trajectory, JKSAS, 41, 921-930 (2013). http://dx.doi.org/10.5139/JKSAS.2013.41.12.950
- Jeong BY, Choi YH, Jo SJ, Bang HC, Terrain aided inertial navigation for precise planetary landing, JKSAS, 38, 673-745 (2010). http://dx.doi.org/10.5139/JKSAS.2010.38.7.673
- JPL (Jet Propulsion Laboratory) [Internet], cited 2013a December 18, available from: http://deepspace.jpl.nasa.gov/dsn
- JPL (Jet Propulsion Laboratory) [Internet], cited 2013b November 2, available from: http://www2.jpl.nasa.gov/basics
- Kim KJ, Lee JH, Seo H, Ju G, Lee SR, et al., An introduction to the lunar and planetary science activities in Korea. AdSpR, Inpress, (2013). http://dx.doi.org/10.1016/j.asr.2013.05.009
- Lee DH, Bang HC, Low thrust, fuel optimal earth escape trajectories design, JKSAS, 35, 647-654 (2007). http://dx.doi.org/10.5139/JKSAS.2007.35.7.647
- Lozier D, Galal K, Folta D, Beckman M, Lunar prospector mission design and trajectory support, in AAS/GSFC International Symposium on Space Flight Dynamics, Greenbelt, MD, 11-15 May 1998, AAS 98-323
- McCarthy K, Carter D, Near Earth Network Users' Guide, Revision 1 (GSFC Greenbelt, Maryland, 2010), 2-1 -10-10.
- No TS, Jeon GE, A study on optimal earth-moon transfer orbit design using mixed impulsive and continuous thrust, JKSAS, 38, 684-692 (2010). http://dx.doi.org/10.5139/JKSAS.2010.38.7.684
- Song YJ, Ahn SI, Choi SJ, Sim ES, Ground contact analysis for Korea's fictitious lunar orbiter mission, JASS, 30, 255-267 (2013). http://dx.doi.org/10.5140/JASS.2013.30.4.255
- Song YJ, Park SY, Choi KH, Shim ES, Development of Korean preliminary lunar mission design software, JKSAS, 36, 357-367 (2008). http://dx.doi.org/10.5139/JKSAS.2008.36.4.357
- Song YJ, Park SY, Choi KH, Sim ES, Optimal earth-moon trajectory design using constant and variable low thrust, JKSAS, 37, 843-854 (2009a). http://dx.doi.org/10.5139/JKSAS.2009.37.9.843
- Song YJ, Park SY, Choi KH, Sim ES, A lunar cargo mission design strategy using variable low thrust, AdSpR, 43, 1391-1406 (2009b). http://dx.doi.org/10.1016/j.asr.2009.01.020
- Song YJ, Park SY, Kim HD, Lee JH, Sim ES, Trans Lunar Injection (TLI) maneuver design and analysis using finite thrust, JKSAS, 38, 998-1011 (2010a). http://dx.doi.org/10.5139/JKSAS.2010.38.10.998
- Song YJ, Park SY, Kim HD, Lee JH, Sim ES, Analysis of Delta-V Losses During Lunar Capture Sequence using Finite Thrust, JASS, 28, 203-216 (2011). http://dx.doi.org/10.5140/JASS.2011.28.3.203
- Song YJ, Park SY, Kim HD, Sim ES, Development of precise lunar orbit propagator and lunar polar orbiter's lifetime analysis, JASS, 27, 97-106 (2010b). http://dx.doi.org/10.5140/JASS.2010.27.2.097
- Song YJ, Woo J, Park SY, Choi KH, Sim ES, The earth moon transfer trajectory design and analysis using intermediate loop orbits, JASS, 26, 171-186 (2009c). http://dx.doi.org/10.5140/JASS.2009.26.2.171
- Vallado DA, Fundamentals of astrodynamics and applications, 3rd ed. (Kluwer Academic Publishers, Boston, 2007), 265-268, 307-311.
- Woo J, Song YJ, Park SY, Kim HD, Sim ES, An earth-moon transfer trajectory design and analysis considering spacecraft's visibility from Daejeon ground station at TLI and LOI maneuvers, JASS, 27, 195-204 (2010). http://dx.doi.org/10.5140/JASS.2010.27.3.195
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