[논문]Analysis on Tracking Schedule and Measurements Characteristics for the Spacecraft on the Phase of Lunar Transfer and Capture

Song, Young-Joo; Choi, Su-Jin; Ahn, Sang-Il; Sim, Eun-Sup

doi:10.5140/jass.2014.31.1.51

Analysis on Tracking Schedule and Measurements Characteristics for the Spacecraft on the Phase of Lunar Transfer and Capture 원문보기

Journal of astronomy and space sciences, v.31 no.1, 2014년, pp.51 - 61

Song, Young-Joo (Korea Aerospace Research Institute) , Choi, Su-Jin (Korea Aerospace Research Institute) , Ahn, Sang-Il (Korea Aerospace Research Institute) , Sim, Eun-Sup (Korea Aerospace Research Institute)

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In this work, the preliminary analysis on both the tracking schedule and measurements characteristics for the spacecraft on the phase of lunar transfer and capture is performed. To analyze both the tracking schedule and measurements characteristics, lunar transfer and capture phases' optimized trajectories are directly adapted from former research, and eleven ground tracking facilities (three Deep Space Network sties, seven Near Earth Network sites, one Daejeon site) are assumed to support the mission. Under these conceptual mission scenarios, detailed tracking schedules and expected measurement characteristics during critical maneuvers (Trans Lunar Injection, Lunar Orbit Insertion and Apoapsis Adjustment Maneuver), especially for the Deajeon station, are successfully analyzed. The orders of predicted measurements' variances during lunar capture phase according to critical maneuvers are found to be within the order of mm/s for the range and micro-deg/s for the angular measurements rates which are in good agreement with the recommended values of typical measurement modeling accuracies for Deep Space Networks. Although preliminary navigation accuracy guidelines are provided through this work, it is expected to give more practical insights into preparing the Korea's future lunar mission, especially for developing flight dynamics subsystem.

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In their work, both the cut-off angle of given typical stations and the orbiter’s Line of Sight (LOS) conditions were considered to determine the ground contact opportunities.
The main goal of this work is to additionally analyze the tracking schedule for the spacecraft on the phases of a lunar transfer and capture which were all omitted phases in the previous study done by Song et al. (2013). Moreover, through this work, expected measurements' characteristics during each phase with critical maneuvers (TLI, LOI and AAM: Apoapsis Adjustment Maneuver) are also predicted and analyzed.

참고문헌 (22)

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

원문보기 상세보기
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

원문보기 상세보기
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

원문보기 상세보기
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

상세보기
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

원문보기 상세보기
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

원문보기 상세보기
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

원문보기 상세보기
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

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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

원문보기 상세보기
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

상세보기
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

원문보기 상세보기
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

원문보기 상세보기
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

원문보기 상세보기
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

원문보기 상세보기
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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Analysis on Tracking Schedule and Measurements Characteristics for the Spacecraft on the Phase of Lunar Transfer and Capture 원문보기

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Analysis on Tracking Schedule and Measurements Characteristics for the Spacecraft on the Phase of Lunar Transfer and Capture 원문보기

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