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Sensitivity Analysis of Initial Error for the Trajectory to the Sun-Earth Libration Point
- WANG Yamin,QIAO Dong,CUI Pingyuan
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School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
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Received |
Revised |
Published |
14 Oct 2014 |
30 Apr 2015 |
20 May 2022 |
Issue Date |
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20 May 2022 |
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References
[1] Canalias E, Gomez G, Marcote M, et al. Assessment of mission design including utilization of libration points and weak stability boundaries[EB/OL].[2014-10-14].http://www.esa.int/act.
[2] Farquhar RW, Dunham D W, Guo Y, et al. Utilization of libration points for human exploration in the Sun-Earth-Moon system and beyond[J]. Acta Astronautica, 2004,55(3):687-700.
[3] Canalias E,Masdemont J J. Computing natural transfers between Sun-Earth and Earth-Moon Lissajous libration point orbits[J]. Acta Astronautica, 2008,63(1):238-248.
[4] Howell K C,Kakoi M. Transfers between the Earth-Moon and Sun-Earth systems using manifolds and transit orbits[J]. Acta Astronautica, 2006,59(1):367-380.
[5] Gómez G, Jorba A, Masdemont J J, et al. Study of the transfer from the Earth to a halo orbit around the equilibrium point L1[J]. Celestial Mechanics and Dynamical Astronomy, 1993,56(4):541-562.
[6] Barden B T, Howell K C, Lo M W. Application of dynamical systems theory to trajectory design for a libration point mission[J]. Journal of the Astronautical Sciences, 1997,45(2):161-178.
[7] Nakamiya M, Scheeres D J, Yamakawa H, et al. Analysis of capture trajectories into periodic orbits about libration points[J]. Journal of Guidance, Control, and Dynamics, 2008,31(5):1344-1351.
[8] Wang Y, Qiao D, Cui P. Analysis of two-impulse capture trajectories into Halo orbits of Sun-Mars system[J]. Journal of Guidance, Control, and Dynamics, 2014,37(3):985-990.
[9] Davis K E, Anderson R L, Scheeres D J, et al. The use of invariant manifolds for transfers between unstable periodic orbits of different energies[J]. Celestial Mechanics and Dynamical Astronomy, 2010,107(4):471-485.
[10] Gómez G,Masdemont J J. Some zero cost transfers between libration point orbits[C]//AAS PAPER 00-177, AAS/AIAA Astrodynamics Specialist Conference. [S.l.]:AAS/AIAA,2000.
[11] Howell K C, Hiday-Johnston L A. Time-free transfers between Libration-Point orbits in the elliptic restricted problem[J]. Acta Astronautica, 1994,32(4):245-254.
[12] Koon W S, Lo M W, Marsden J E, et al. Shoot the Moon[C]//AAS/AIAA Space Flight Mechanics Meeting. Clearwater, Florida: AAS/AIAA, 2000.
[13] Koon W S, Lo M W, Marsden J E, et al. Low energy transfer to the Moon[J]. Celestial Mechanics and Dynamical Astronomy, 2001(81):6373.
[14] Gómez G, Koon W S, Lo M W, et al. Connecting orbits and invariant manifolds in the spatial three-body problem[J]. Nonlinearity, 2004,17(5):1571-1606.
[15] Gómez G,Koon W S, Lo M W, et al. Invariant manifolds, the spatial three-body problem and space mission design[D].[S. l.]: AAS, 2001.
[16] Parker J S,Lo M W.Shoot the Moon 3D[C]//AAS/AIAA Astrodynamics Specialists Conference. Lake Tahoe. California: AAS/AIAA, 2005.
[17] Wu W R, Liu Y, Liu L, et al. Pre-LOI trajectory maneuvers of the Chang'e-2 libration point mission[J]. Science China Information Sciences, 2012,55(6):1249-1258.
[18] Qiao D, Cui P Y, Wang Y M, et al. Design and analysis of an extended mission of CE-2: From lunar orbit to Sun-Earth L2 region[J]. Adv Space Res, 2014,54(10):2087-2093.
[19] 吴伟仁,崔平远,乔栋,等.嫦娥二号日地拉格朗日L2点探测轨道设计与实施[J].科学通报,2012,57:1987-1991.[Wu W R, Cui P Y, Qiao D, et al. Design and performance of exploring trajectory to Sun-Earth L2 point for Chang'E-2 mission[J]. Chin Sci Bull (Chin Ver), 2012,57:1987-1991.]
[20] Masaki N,Kawakatsu Y. Transfer trajectories from the Moon to Sun-Earth halo orbits[J]. Journal of Guidance, Control, and Dynamics, 2014,37(3):1000-1003.