1 |
송영주, 박상영, 최규홍, 심은섭, “한국형 달탐사 임무 예비 설계 소프트웨어의 개발”, 한국항공우주학회지, 제36권 4호, pp. 357-368, 2008.
|
2 |
Perkins, F. M., “Flight Mechanics ofLow-Thrust Spacecraft”, Journal of AerospaceScience, Vol. 26, pp. 291-297, 1959.
|
3 |
Edelbaum, T. N., “Propulsion Requirementsfor Controllable Satellites”, ARS Journal, Vol. 31,pp. 1079-1089, 1961.
DOI
|
4 |
Oleson, S. R., "Mission Advantages of ConstantPower, Variable Isp Electrostatic Thrusters", NASATechnical Memo 2000-210477, 2000.
|
5 |
Russell, C. T., Abshire, J., A'Hearn, M., Arnold, J., Elphic, R. C., Head, J., Pieters, C., Hickman, M., Palac, D., Kluever, C., Konopliv, A., Metzger, A., Sercel, J., McCord, T., Phillips, R. J., Purdy, W., Rosenthal, R., and Sykes, M., “A Solar Electric Propulsion Mission to the Moon and Beyond", Journal of Advances in Space Research, Vol. 18, pp. 75-80, 1996.
DOI
ScienceOn
|
6 |
Enright, P. J. and Conway, B. A., “DiscreteApproximations to Optimal Trajectories UsingDirect Transcription and Nonlinear Programming”,Journal of Guidance, Control, Dynamics, Vol.15, pp. 994-1002, 1992.
DOI
|
7 |
Pierson, B. L. and Kluever, C. A.,"Three-Stage Approach to Optimal Low-ThrustEarth-Moon Trajectories", Journal of Guidance,Control, Dynamics, Vol.17, pp. 1275-1282, 1994.
DOI
ScienceOn
|
8 |
Kluever, C. A. and Pierson, B. L.,"OptimalLow-Thrust Three-Dimensional Earth-MoonTrajectories", Journal of Guidance, Control,Dynamics, Vol. 18, pp. 830-837, 1995.
DOI
ScienceOn
|
9 |
Kluever, C. A. and Pierson, B. L.,"OptimalEarth-Moon Trajectories Using Nuclear ElectricPropulsion, Jouranl of Guidance, Control,Dynamics, Vol. 20, pp. 239-245, 1997.
DOI
ScienceOn
|
10 |
Herman, A. L. and Conway, B. A.."Optimal, Low-Thrust, Earth-Moon OrbitTransfer", Journal of Guidance, Control,Dynamics, Vol. 21, pp. 141-147, 1998.
DOI
ScienceOn
|
11 |
Betts, J. T., and Erb, S. O., "Optimal Low Thrust Trajectories to the Moon", Journal of Applied Dynamical Systems, Vol.2, pp. 144-170, 2003.
DOI
|
12 |
Foing, B. H., Racca, G.D., Marini, A.,Evrard, E., Stagnaro, L., Almeida, M., Koschny, D.,Frew, D., Zender, J., Heather, J., Grande, M.,Huovelin, J., Keller, H.U., Nathues, A., Josset, J.L.,Malkki, A., Schmidt, W., Noci, G., Birkl, R., Iess,L., Sodnikk, Z. and McManamonk, P., “SMART-1Mission to the Moon: Status, First Results andGoals”, Advances in Space Research, Vol. 37,pp. 6-13, 2006.
DOI
ScienceOn
|
13 |
Raymana, M. D., Varghese, P., Lehman, D. H. and Livesayet L. L., “Results from the Deep Space 1 Technology Validation Mission”, Acta Astronautica, Vol. 47, pp. 475-487, 2000.
DOI
ScienceOn
|
14 |
Raymana, M, D., Fraschettia, T. C.,Raymonda, C., A. and Russellb, C. T.,"Dawn:Amission in development for explorationof main belt asteroids Vesta and Ceres",Acta Astronautica, Vol. 58, pp. 605-616, 2006.
DOI
ScienceOn
|
15 |
Kawaguchi, J., Kuninaka, H., Fujiwara,A. and Uesugi, T, "MUSES-C, Its launch andearly orbit operations", Acta Astronautica,Vol.59, pp. 669-678, 2006.
DOI
ScienceOn
|
16 |
King, D. Q., de Grys, K. H., andJankovsky, R., "Multi-Mode Hall ThrusterDevelopement", AIAA paper 2001-3778, 2001.
|
17 |
Fisch, N. J., Raitses, Y., Dorf, L. A. andLitvak, A. A.,"Variable Operation of HallThruster with Multiple Segmented Electrodes",Journal of Applied Physics, Vol. 89, pp.2040-2046, 2001.
DOI
ScienceOn
|
18 |
Goebel, D. M., Brophy, J. R., Polk, J. E.,Katz, I. and Anderson, J., "Variable SpecificImpulse High Power Ion Thruster", AIAA paper2005-4246, 2005.
|
19 |
Chang-Diaz, F. R., Squire, J. P., Glover,T., Petro, A. J., Bering, E. A., Baity, F. W,Goulding, R. H., Carter, M. D., Bengtson, R. D.and Breizman, B. N., "The VASIMR Engine:Project Status and Recent Accomplishments",Presented at the 42th Aerospace SciencesMeeting and Exhibit, Reno, NV, Jan. 5-8, 2004.
|
20 |
Bering, E. A., Chang-Diaz, F. R., Squire, J. P., Brukardt, M., Glover, T. W., Bengtson, R. D., Jacobson, V. T., McCaskill, G. E. and Cassady, L., "Electromagnetic Ion Cyclotron Resonance Heating in the VASIMR", Advance in Space Research, Vol. 42, pp. 192-205, 2008.
DOI
ScienceOn
|
21 |
Kluever, C. A., “Geostationary Orbit Transfers Using Solar Electric Propulsion with Specific Impulse Modulation”, Journal of Spacecraft and Rockets, Vol. 41, pp. 461-466, 2004.
DOI
ScienceOn
|
22 |
Casalino, L. and Colasurdo, G.,"Improved Edelbaum’s Approach to OptimizeLow Earth/Geostationary Orbits Low-ThrustTransfers", Journal of Guidance, Control, andDynamics, Vol. 30, pp. 1504-1510, 2007.
DOI
ScienceOn
|
23 |
Casalino, L. and Colasurdo, G., "Optimizationof Variable-Specific-Impulse Interplanetary Trajectories",Journal of Guidance, Control, and Dynamics,Vol. 27, pp. 678-684, 2004.
DOI
ScienceOn
|
24 |
Chang-Diaz, F. R., Hsu, M. M., Braden,E., Johnson, IL. and Yang, T. F., “Rapid MarsTransits with Exhaust-Modulated PlasmaPropulsion”, NASA Technical Paper 3539, 1995.
|
25 |
Vadali, S. R., Nah, R., Braden, E. andJohnson, IL., “Fuel-Optimal Planer Earth-MarsTrajectories Using Low-Thrust Exhaust-ModulatedPropulsion”, Journal of Guidance, Control,Dynamics, Vol. 23, pp. 476-482, 2000.
DOI
ScienceOn
|
26 |
Nah, R. Vadali, S. R., Braden, E. " Fuel -Optimal, Low-Thrust, Three-DimensionalEarth-Mars Trajectories", J. Guidance, Control,and Dynamics, Vol. 24, pp. 1100-1107, 2001.
DOI
ScienceOn
|
27 |
Park, S.-Y. and Mazanek, D. D., "Missionfunctionality for deflecting Earth-crossing asteroids/comets", Journal of Guidance, Controland Dynamics, Vol. 26, pp. 734-742, 2003.
DOI
ScienceOn
|
28 |
Park, S.-Y., Seywald, H., Krizan, S. A.and Stillwagen, F. H., “Mission Design forHuman Outer Planet Exploration (HOPE) usinga Magnetoplasma Spacecraft”, Planetary andSpace Science, Vol. 54. pp. 737-749, 2006.
DOI
ScienceOn
|
29 |
Golan, O. M. and Breakwell, J. V.,"Minimum Fuel Lunar Trajectories for aLow-Thrust Power-Limited Spacecraft",Dynamics and Control, Vol. 4, pp. 383-394,1994.
DOI
|
30 |
Song, Y.-J., Park, S.-Y., Choi, K.-H. andSim, E.-S., "A Lunar Cargo Mission DesignStrategy using Variable Low Thrust", Advancesin Space Research, Vol. 43, pp. 1391-1406, 2009.
DOI
ScienceOn
|
31 |
Park, S.-Y. and Mazanek, D. D.,"Deflection of Earth-crossing asteroids/cometsusing rendezvous spacecraft and laser ablation",Journal of Astronautical Sciences, Vol. 53,pp. 21-37, 2005.
|
32 |
Song, Y.-J., Park, S.-Y., and Choi, K.-H.,“Optimal Deflection of Earth-Crossing Objectsusing a Power Limited Spacecraft,” 17thAAS/AIAA Space Flight Mechanics Meeting,Sedona, Arizona, Paper AAS 07-147, 2007.
|
33 |
Park, S.-Y. and Choi, K-H., "Optimallow-thrust intercept/rendezvous trajectories toEarth-crossing objects", Journal of Guidance,Control and Dynamics, Vol. 28, pp. 1049-1055,2005.
DOI
ScienceOn
|
34 |
이동헌, 방효충, “저추력기를 이용한 연로최적의 지구 탈출 궤적 설계 연구”, 한국항공우주학회지, 제35권 제7호, pp. 647-654, 2007.
|
35 |
이동헌, 최윤혁, 방효충, “2차원의 달 진입 최적 궤적 설계”, 한국항공우주학회 추계학술 발 표 논문집, KSAS08-2946, 2008.
|
36 |
송영주, 박상영, 최규홍, 심은섭, “등저추력을 이용한 최적의 달탐사 비행궤적 설계”, 한국항공우주학회 추계학술 발표회 논문집, KSAS08-2944, 2008.
|
37 |
Shannon, J., "The Clementine Satellite",Energy and Technology Review, June 1994.
|
38 |
Boden, D. G. and Hoffman, S., J., OrbitSeletion and Astrodyanmcis, in Larson, W. J.and Pranke, L., K. (eds.) Human Spaceflight:Mission Analysis and Design, McGraw-Hill, NewYork, pp. 244-255, 1999.
|
39 |
Betts, J. T., Practical Method for OptimalControl Using Nonlinear Programming, SIAM,Philadelphia, pp. 147-149, 2001.
|
40 |
The Boeing Company, "SOCS Release6.4", M&CT-TECH-01-014, 2005.
|
41 |
Seywald, H. Roithmayr, C. M.,Troutman, P. A. and Park, S.-Y. “Fuel-OptimalTransfers Between Coplanar Circular OrbitsUsing Variable-Specific-Impulse Engines”,Journal of Guidance, Control, and Dynamics,Vol. 28, pp. 795-800, 2005.
DOI
ScienceOn
|
42 |
La Mantia, M., Casalino, L. "Indirectoptimization of low-thrust capture trajectories",Journal of Guidance, Control, and Dynamics,Vol. 29, pp. 1011-1014, 2006.
DOI
ScienceOn
|
43 |
Tooley, C., "Lunar Reconnaissance OrbiterProject Overview & Status", NASA Goddard SpaceFlight Center, http://lunar.gsfc.nasa.gov/301.286.1158,2006.
|
44 |
Ranieri, C., and Ocampo, C. A., "IndirectOptimization of Low Earth Orbit to LowLunar Orbit Transfers", AIAA paper 2008-7075,2008.
|
45 |
Lozier, D., Galal, K., Folta, D., andBeckman, M., "Lunar Prospector MissionDesign and Trajectory Support", AAS 98-323,pp. 297–311, 1998.
|