Analysis of Delta-V Losses During Lunar Capture Sequence Using Finite Thrust |
Song, Young-Joo
(Space Application and Future Technology Center, Korea Aerospace Research Institute)
Park, Sang-Young (Astrodynamics and Control Laboratory, Department of Astronomy, Yonsei University) Kim, Hae-Dong (Space Application and Future Technology Center, Korea Aerospace Research Institute) Lee, Joo-Hee (Space Application and Future Technology Center, Korea Aerospace Research Institute) Sim, Eun-Sup (Space Application and Future Technology Center, Korea Aerospace Research Institute) |
1 | Kato M, Sasaki S, Tanaka K, Iijima Y, Takizawa Y, The Japanese lunar mission SELENE: science goals and present status, AdSpR, 42, 294-300 (2008). http://dx.doi.org/10.1016/j.asr.2007.03.049 DOI |
2 | Zheng Y, Ouyang Z, Li C, Liu J, Zou Y, China's lunar exploration program: present and future, P&SS, 56, 881-886 (2008). http://dx.doi.org/10.1016/j.pss.2008.01.002 DOI |
3 | Tanaka S, Shiraishi H, Kato M, Okada T, The science objectives of the SELENE-II mission as the post SELENE mission, AdSpR, 42, 394-401 (2008). http://dx.doi.org/10.1016/j.asr.2007.07.002 DOI |
4 | The Boeing Company, SOCS user's guide release 7.0.2, M&CT-TECH-01-104 (The Boeing Company, Seattle, 2010), 529-543. |
5 | Vallado DA, McClain WD, Fundamentals of astrodynamics and applications, 3rd ed. (Kluwer Academic Publishers, Boston, 2007), 33-36. |
6 | Walker MJH, Ireland B, Owens J, A set modified equinoctial orbit elements, CeMec, 36, 409-419 (1985). http://dx.doi.org/10.1007/BF01227493 DOI |
7 | 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 DOI ScienceOn |
8 | 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 DOI |
9 | Song YJ, Park SY, Choi KH, Sim ES, A lunar cargo mission design strategy using variable low thrust, AdSpR, 43, 1391-1406 (2009a). http://dx.doi.org/10.1016/j.asr.2009.01.020 DOI |
10 | Standish EM, JPL planetary and lunar ephemerides, DE405/LE405 (Jet Propulsion Laboratory, Los Angeles, 1998), 1-6. |
11 | Song YJ, Park SY, Choi KH, Sim ES, Optimal earth-moon trajectory design using constant and variable low thrust, J. Korean Soc. Aeronaut. Sci., 37, 843-854 (2009b). 과학기술학회마을 DOI ScienceOn |
12 | Song YJ, Park SY, Kim HD, Joo HL, Sim ES, Trans Lunar Injection (TLI) maneuver design and analysis using finite thrust, J. Korean Soc. Aeronaut. Sci., 38, 998-1011 (2010a). 과학기술학회마을 DOI ScienceOn |
13 | 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 DOI ScienceOn |
14 | Kechichian JA, Minimum-time constant acceleration orbit transfer with first-order oblateness effect, JGCD, 23, 595-603 (2000). DOI ScienceOn |
15 | Song YJ, Park SY, Choi KH, Sim ES, Development of Korean preliminary lunar mission design software, J. Korean Soc. Aeronaut. Sci., 36, 357-367 (2008). 과학기술학회마을 DOI |
16 | Lee DH, Bang HC, Low thrust, fuel optimal earth escape trajectories design, J. Korean Soc. Aeronaut. Sci., 35, 647-654 (2007). 과학기술학회마을 DOI |
17 | Lozier D, Galal K, Folta D, Beckman M, Lunar pospector mission design and trajectory support (AAS 98-323), in Proceedings of the AAS/GSFC International Symposium on Space Flight Dynamics, Greenbelt, MD, 11-15 May 1998, 297-311. |
18 | No TS, Jeon GE, A study on optimal earth-moon transfer orbit design using mixed impulsive and continuous thrust, J. Korean Soc. Aeronaut. Sci., 38, 684-692 (2010). 과학기술학회마을 DOI ScienceOn |
19 | Chin G, Brylow S, Foote M, Garvin J, Kasper J, et al., Lunar Reconnaissance Orbiter overview: the instrument suite and mission, SSRv, 129, 391-419 (2007). http://dx.doi.org/10.1007/s11214-007-9153-y DOI |
20 | Betts JT, Practical methods for optimal control and estimation using nonlinear programming, 2nd ed. (Society for Industrial and Applied Mathematics, Philadelphia, 2010), 152-165. |
21 | Cho DH, Jeong BY, Lee DH, Bang HC, Optimal perilune altitude of lunar landing trajectory, IJASS, 10, 67-74 (2009). 과학기술학회마을 DOI |
22 | Cho DH, Jung YS, Lee DH, Jung BY, Bang HC, Satellite trajectory correction maneuver for lunar mission based on three-body dynamics, J. Korean Soc. Aeronaut. Sci., 38, 875-881 (2010). 과학기술학회마을 DOI |
23 | Goswamia JN, Annaduraib M, Chandrayaan-1 mission to the Moon, AcAau, 63, 1215-1220 (2008). http://dx.doi.org/10.1016/j.actaastro.2008.05.013 DOI |
24 | Jeong BY, Choi YH, Jo SJ, Bang HC, Terrain aided inertial navigation for precise planetary landing, J. Korean Soc. Aeronaut. Sci., 38, 673-745 (2010). 과학기술학회마을 DOI |
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