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Design of communication relay mission for supporting lunar-farside soft landing

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  • Special Focus on Deep Space Communications
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Abstract

Chang’E-IV will be the first soft-landing and rover mission on the lunar farside. The relay satellite, which is located near the Earth-Moon L2 point for relay communication, is the key to the landing mission. Based on an analysis of the characteristics of the task and the technical difficulties associated with the relay satellite system, the overall design scheme of the relay communication mission is proposed in terms of trajectory design and communication system design among other aspects. First, according to the complex dynamic environment, a mission orbit that serves as an uninterrupted communication link is presented. A short-duration and low-energy transfer trajectory with lunar flyby is discussed. Orbital correction and a low-cost control strategy for orbit maintenance in the Earth-Moon L2 point region are provided. Second, considering the existing technical constraints, the requirement of relay communication in different stages and the design schemes of frequency division and redundant relay communication system are introduced. Finally, based on the trajectory design index and the performance of the communication system, the overall design scheme of the relay communication mission is proposed. This mission will provide the technical support and reference required for the Chang’E-IV mission.

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References

  1. Farquhar R W, Dunham D W, Guo Y, et al. Utilization of libration points for human exploration in the Sun-Earth-Moon system and beyond. Acta Astronaut, 2004, 55: 687–700

    Article  Google Scholar 

  2. Dunham D W, Farquhar R W, Eysmont N, et al. Interplanetary human exploration enabled by lunar swingbys and libration-point orbits. In: Proceedings of AIAA/AAS Astrodynamics Specialist Conference, San Diego, 2014

    Google Scholar 

  3. Burns J O, Kring D A, Hopkins J B, et al. A lunar L2 far side exploration and science mission concept with the orion multi-purpose crew vehicle and a teleported lander/rover. Adv Space Res, 2012, 52: 306–320

    Article  Google Scholar 

  4. Mimoun D, Wieczorek M A, Alkalai L, et al. Far side explorer: unique science from a mission to the far side of the Moon. Exp Astron, 2012, 33: 529–585

    Article  Google Scholar 

  5. Farquhar R W. Lunar communications with libration-point satellites. J Spacecr Rocke, 1967, 4: 1383–1384

    Article  Google Scholar 

  6. Farquhar R W. The Control and Use of Libration-Point Satellites. NASA Technical Report NASA TR R-346, 1970

    Google Scholar 

  7. Farquhar R W. The Utilization of Halo Orbits in Advanced Lunar Operations. NASA Technical Note NASA TN D-6365, 1971

    Google Scholar 

  8. Tang Y H, Wu W R, Qiao D, et al. Effect of orbital shadow at an Earth-Moon Lagrange point on relay communication mission. Sci China Inf Sci, 2017, 60: 112301

    Article  Google Scholar 

  9. Farquhar R W, Kamel A A. Quasi-periodic orbits about the trans-lunar libration point. Celest Mech Dyn Astron, 1973, 7: 458–473

    Article  MATH  Google Scholar 

  10. Richardson D L. Analytic construction of periodic orbits about the collinear points. Celest Mech Dyn Astron, 1980, 22: 241–253

    Article  MathSciNet  MATH  Google Scholar 

  11. Dutt P, Sharma R K. Analysis of periodic and quasi-periodic orbits in the Earth-Moon system. J Guid Control Dyn. 1971, 33: 1010–1017

    Google Scholar 

  12. Howell K C. Families of orbits in the vicinity of the collinear libration points. In: Proceedings of AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Boston, 1998

    Google Scholar 

  13. Gómez G, Mondelo J M. The dynamics around the collinear equilibrium points of the RTBP. Phys D Nonlinear Phenom, 2001, 157: 283–321

    Article  MathSciNet  MATH  Google Scholar 

  14. Grebow D J. Generating periodic orbits in the circular restricted three body problem with applications to lunar south pole coverage. Dissertation for Ph.D. Degree. West Lafayette: Purdue University, 2006

    Google Scholar 

  15. Parker J S, Born G H. Direct lunar halo orbit transfers. J Astronaut Sci, 2008, 56: 441–476

    Article  Google Scholar 

  16. Rowells M. Development of a long-term Earth-Moon trans-lunar libration point orbit. In: Proceedings of AIAA Space Conference and Exposition, Pasadena, 2012

    Google Scholar 

  17. Geraldo M O, Prado A F, Sanchez D M, et al. Traveling between the Earth-Moon lagrangian points and the earth. In: Proceedings of SpaceOps Conference, Daejeon, 2015

    Google Scholar 

  18. Gordon D P. Transfers to Earth-Moon L2 halo orbits using lunar proximity and invariant manifolds. Dissertation for Ph.D. Degree. West Lafayette: Purdue University, 2008

    Google Scholar 

  19. Li M, Zheng J. Impulsive lunar halo transfers using the stable manifolds and lunar flybys. Acta Astronaut, 2010, 66: 1481–1492

    Article  Google Scholar 

  20. 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. Chin Sci Bull, 2012, 57: 1987–1991

    Article  Google Scholar 

  21. Parker J S. Families of low-energy lunar halo transfers. In: Proceedings of AAS/AIAA Spaceflight Dynamics Conference, Tampa, 2006

    Google Scholar 

  22. Koon W S, Lo M W, Marsden J E, et al. Low energy transfer to the moon. Celest Mech Dyn Astron, 2001, 81: 63–73

    Article  MathSciNet  MATH  Google Scholar 

  23. Lo M W, Ross S D. The lunar L1 gateway: portal to the stars and beyond. In: Proceedings of AIAA Space Conference and Exposition, Albuquerque, 2001

    Google Scholar 

  24. Alessi E M, Gomez G, Masdemont J J. LEO-Lissajous transfers in the Earth-Moon system. In: Proceedings of the 59th International Astronautical Federation Congress, Glasgow, 2008

    Google Scholar 

  25. Howell K C, Lo M W, Barden B T. Application of dynamical systems theory to trajectory design for a libration point mission. In: Proceedings of AIAA Astrodynamics Conference, San Diego, 1996. 161–178

    Google Scholar 

  26. Pergola P, Ruggiero A, Casaregola C, et al. Chemical and electric transfers to Earth-Moon halo orbits. In: Proceedings of the 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Diego, 2013. 116–128

    Google Scholar 

  27. Howell K C, Pernicka H J. Station-keeping method for libration point trajectories. J Guid Control Dyn, 1990, 16: 713–723

    Google Scholar 

  28. Pavlak T, Howell K. Strategy for long-term libration point orbit station keeping in the Earth-Moon system. In: Proceedings of AAS/AIAA Astrodynamics Specialist Conference, Girdwood, 2011

    Google Scholar 

  29. Pavlak T, Howell K C. Strategy for optimal, long-term stationkeeping of libration point orbits in the Earth-Moon system. In: Proceedings of AIAA/AAS Astrodynamics Specialist Conference, Minneapolis, 2013. 199–208

    Google Scholar 

  30. Folta D, Woodard M, Cosgrove D. Stationkeeping of the first Earth-Moon libration orbiters: the ARTEMIS mission. In: Proceedings of AAS/AIAA Astrodynamics Specialist Conference, Girdwood, 2011

    Google Scholar 

  31. Simó C, Gómez G, Llibre J, et al. On the optimal station keeping control of halo orbits. Acta Astron, 1987, 15: 391–397

    Article  Google Scholar 

  32. Kulkarni J, Campbell M. Asymptotic stabilization of motion about an unstable orbit: application to spacecraft flight in halo orbit. In: Proceedings of American Control Conference, Boston, 2004. 1025–1030

    Google Scholar 

  33. Xin M, Dancer M, Balakrishnan S, et al. Station keeping of an L2 libration point satellite with θ-D technique. In: Proceeding of the 2004 American Control Conference, Boston, 2004

    Google Scholar 

  34. Colombo G. The stabilization of an artificial satellite at the inferior conjunction point of the Earth-Moon system. J Astron Sci, 1961, 6: 213–222

    Google Scholar 

  35. Zhou H, Li H T, Dong G L. Relative position determination between Chang’E-3 lander and rover using in-beam phase referencing. Sci China Inf Sci, 2015, 58: 092201

    Google Scholar 

  36. Wu W R, Luo H, Chen M, et al. Design and experiment of deep space telemetry and data transmission system in libration points 2 exploring. Syst Eng Electron, 2012, 34: 2559–2563

    Google Scholar 

  37. Wu W R, Huang L, Jie D G, et al. Design and experiment of X-band TT&C system for the project of CE-2. Sci Sin Inform, 2011, 41: 1171–1183

    Google Scholar 

  38. Wu W R, Dong G L, Li H T, et al. Engineering and Technology of Deep Space measurement and Control Communication System (in Chinese). Beijing: Science Press, 2013

    Google Scholar 

  39. Gao L, Zhang S, Liu Z Y, et al. An overview of multi-antenna technologies for space-ground integrated networks. Sci China Inf Sci, 2016, 59: 121301

    Article  Google Scholar 

Download references

Acknowledgements

This work was supported by National Science and Technology Major Project of the Ministry of Science and Technology of China (Lunar Exploration Program), National Natural Science Foundation of China (Grant No. 11572038), and Chang Jiang Scholars Program.

Author information

Authors and Affiliations

  1. Lunar Exploration Program and Space Engineering Center, Beijing, 100190, China

    Weiren Wu & Yuhua Tang

  2. School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081, China

    Yuhua Tang & Dong Qiao

  3. Dong Fang Hong Satellite Co. Ltd., Beijing, 100084, China

    Lihua Zhang

  4. Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing, 100081, China

    Dong Qiao

Authors
  1. Weiren Wu
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  2. Yuhua Tang
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  3. Lihua Zhang
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  4. Dong Qiao
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Corresponding author

Correspondence to Dong Qiao.

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Wu, W., Tang, Y., Zhang, L. et al. Design of communication relay mission for supporting lunar-farside soft landing. Sci. China Inf. Sci. 61, 040305 (2018). https://doi.org/10.1007/s11432-017-9202-1

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  • DOI: https://doi.org/10.1007/s11432-017-9202-1

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