Target Selection and Trajectory Design for Manned Asteroid Missions

SHANG Haibin1, CUI Pingyuan2, XIONG Xu3, WU Xiaoyu4

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Journal of Deep Space Exploration ›› 2014, Vol. 1 ›› Issue (1) : 36-43.
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Article

Target Selection and Trajectory Design for Manned Asteroid Missions

  • SHANG Haibin1, CUI Pingyuan2, XIONG Xu3, WU Xiaoyu4
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Abstract

In this paper, the target selection and trajectory optimization is investigated for manned asteroid exploration mission in 2020一2040. Firs街,According to various factors and constraints , such as absolute magnitude and orbital parameters, 20 potential candidates for manned missions are presented. And then, the design model for manned mission is constructed, and the exploration trajectories for asteroid candidates are computed场using parameters optimization algorithm directly. Furthermore, the prime vector theory is used to obtain the optimal exploration trajectories. This research can provide valuable proposals for future manned asteroid missions

Keywords

near-earth asteroid / asteroid exploration / manned exploration / target selection / trajectory optimization

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SHANG Haibin, CUI Pingyuan, XIONG Xu, WU Xiaoyu. Target Selection and Trajectory Design for Manned Asteroid Missions. Journal of Deep Space Exploration, 2014, 1(1): 36‒43

References

[1] Qiao D, Cui P Y, Wang Y M. Opportunity options for rendezvous,flyby and sample return mission to different spectral-type asteroids for the 2015-2025[J]. Acts Astronautics, 2012, 72; 143-155.
[2] Ralph K, Gerhard H, Ekkehard K.Optimal deflection of NEOs en mute of collision with the Earth[J]. Icarus, 2006, 182(2):482-488.
[3] Ahrens T J, Harris A W. Deflection and fragmentation of near earth asteroids[J]. Nature (London),1992,360(6403):429-433.
[4] 徐伟彪,赵海斌.小行星深空探测的科学意义和展望[J].地球科学进展,2005,20(11):1184-1185.[Xu W B, ZhaoH B. The scientific significance and prospects of the asteroid exploration[J].Advances in Earth Science, 2005,20(11):1184-1185.]
[5] Cui P Y, Qiao D, Cui H T, et al. Target selection and transfer trajectories design for exploring asteroid mission[J].Sci China Tech Sci, 2010, 53:1150一1158.
[6] Damario L A, Bymes D V. Interplanetary trajectory design for the Galileo mission[C].Reno, NV; American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting,21 st, 1983:10-13.
[7] Jim V M. Postlaunch contingency trajectories for the near-earth asteroid rendezvous mission[J].Journal of Guidance, Contml,and Dynamics, 1997, 20(4):819-823.
[8] Ettore P, Alessandro R, Giovanni B V. Basic targeting strategies for rendezvous and flyby missions to the near-earth asteroids[J].Planetary and Space Science, 2001,49(1):3-22.
[9] Junichiro K, Akira F, Tono U. Hayabusa-its technology and science accomplishment summary and Hayabusa-2[J].Acta Astronautica, 2008,62(10一11):639-647.
[10] 乔栋,黄江川,崔平远,等.嫦娥二号卫星飞越Toutatis小行星转移轨道设计[J].中国科学:技术科学,2013, 43:487-492.[Qiao D, Huang J C, Cui P Y, et al. The orbit design of Chang'e-2 satellite flyby asteroid Toutatis[J].Chinese Science:Science and Technology, 2013,43:487-492.]
[11] Zhu M H, Fa W Z, Huang J C, et al. Morphology of asteroid (4179) Toutatis as imaged by Chang'e-2 spacecraft[J].Geophysical, Research Letter, 2014, 41.
[12] Zimmer A K, Messerschmid E. Going beyond; target selection and mission analysis of human exploration missions to near-earth asteroids[J].Acta Astronautica, 2011,69:1096-1109.
[13] Bradley N, Ocampo C. Optimal free-return trajectories to near-earth asteroids[J].Journal of Guidance, Control, and Dynamics, 2013,36(5):1346-1355.
[14] Hopkins J, Dissel A, Jones M, et al. Plymouth rock an early human mission to near earth asteroids using orion spacecraft[R].Lockheed Martin, 2010.
[15] LeCompte M A, Meyer T R, Horsewood),et al. Early, short-duration, near-earth-asteroid rendezvous missions[J]. Journal of Spacecraft and Rockets, 2012, 49(4):731-741.
[16] Sam W, Bong W. Robotic and human exploration/deflection mission design for asteroid 99942 Apophis[J].Acta Astronautica, 2013,90(1):72-79.
[17] Ivashikin V V, Krylov I V, Lan A. Optimum trajectories for spacecraft mission to asteroid Apophis with a return to the Earth[J].Solar System Research, 2013,47(4):334-345.
[18] Bueskens C, Maurer H. SQP-methods for solving optimal control problems with control and state constraints:adjoint variables, sensitivity analysis and real-time[J.Journal of Computational and Applied Mathematics, 2000,120(1):85一108.
[19] Bruce A C. Spacecraft trajectory optimization}M.New York Cambridge University Press, 2010; 17-20.
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