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Conceptual Design of Ejection, Aerostat and Rolling Group Detectors

  • Qunzhi Li
  • Chao MaEmail author
  • Wangjun Zhang
  • Han Wang
  • Zhihui Zhao
Conference paper
Part of the Lecture Notes in Computer Science book series (LNCS, volume 11743)

Abstract

Floating exploration in near Mars is a new mode between orbiting detection and landing detection, synthesized with the advantages of orbiter’s global coverage and rover’s high image definition. Rolling exploration on Martian surface has the better characteristic of anti-tilting than mature wheeled roaming detection on Martian surface presently. It can adapt to complex environment of Martian surface. Combined with the two new modes, floating exploration technology in near Mars and rolling exploration technology on Martian surface is presented. By Joint exploration of ejection, aerostat and rolling group detectors, the larger ranges and higher accuracy of extraterrestrial three-dimensional stereo-exploration is achieved. It has the characteristics of various exploration mode, multi-dimension, low cost and high reliability.

Keywords

Mars Exploration Ejection Aerostat detection Rolling detection Group detectors 

Notes

Acknowledgment

This research was supported, in part, by the National Natural Science Foundation of China (No. 51875393) and by the China Advance Research for Manned Space Project (No. 030601).

References

  1. 1.
    Tian, L.L., Fang, X.D.: NASA aerospace research and progress, space return and remote sensing, vol. 33, no. 1, p. 81, February 2012Google Scholar
  2. 2.
    Heun, M.K., Cathey, H.M., Haberle Jr., R.: Mars balloon trajectory model for mars geo-science aerobot development, p. 1500, AIAA (1997)Google Scholar
  3. 3.
    Jeffery, L.H., Michael, T.P., Viktor, V.K.: Mars balloon flight test results. In: AIAA Balloon Systems Conference, Seattle, Washington, pp. 1–12 (2009)Google Scholar
  4. 4.
    Fairbrother, D.A.: Development of planetary balloons. In: NASA Goddard Space Flight Center’s Wallops Flight Facility, Balloon Program Office, Code 820, Wallops Island, VA, USA (2007)Google Scholar
  5. 5.
    Lei, Y.P., Yang, C.X.: Research on temperature distribution of mars overpressure balloon. J. Aeronaut. Sch. Aeronaut. Sci. Eng. 33(2), 234–241 (2012). Beijing University of Aeronautics and AstronauticsGoogle Scholar
  6. 6.
    Zhou, C.Q., Min, C.H., Wu, X.Y., et al.: The influence of ground wind on the selection of sounding balloon sites. Guizhou Meteorol. 30(6), 30–32 (2006)Google Scholar
  7. 7.
    Bicchi, A., Balluchi, A., Prattichizzo, D., et al.: Introducing the sphericle: an experimental testbed for research and teaching in nonholonomy. In: Proceedings of the IEEE International Conference on Robotics and Automation, pp. 2620–2625 (1997)Google Scholar
  8. 8.
    Bhattacharya, S., Agrawal, S.K.: Spherical rolling robot: a design and motion planning studies. IEEE Trans. Robot. Autom. 16(6), 835–839 (2000)CrossRefGoogle Scholar
  9. 9.
    Bruhn, E.C., Pauly, K., Kaznov, V.: Extremely low mass spherical rovers for extreme environments and planetary exploration enabled with mems. In: Proceedings of the 8th International Symposium on Artifical Intelligence Robotics and Automation in Space-iSAIRAS, Munich, Germany (2005)Google Scholar
  10. 10.
    Otani, T., Urakubo, T., Maekawa, S., et a1.: Position and attitude control of a spherical rolling robot equipped with a gyro. In: IEEE AMC 2006, Istanbul, Turkey, pp. 416–421 (2006)Google Scholar
  11. 11.
    Hajos, G.A.: An overview of wind-driven rovers for planetary exploration, NASA, Langley Research Center, Hampton, VA (2005)Google Scholar
  12. 12.
    Munk, J.R.: StratSat-the wireless solution. In: The 3rd Stratospheric Platform Systems Workshop, Tokyo, pp. 45–51(2001)Google Scholar
  13. 13.
    Liu, D.L.: Research on motion analysis and control technology of a spherical mobile robot. Ph.D. Dissertation, Beijing University of Posts and Telecommunications (2009)Google Scholar
  14. 14.
    Onda, M., Morikawa, Y.: High-altitude lighter-than-air powered platform. Soc. Automot. Eng. Trans. 16(1), 2216–2223 (1991)Google Scholar
  15. 15.
    Onda, M.: A ground-to airship microwave power transmission experiment for stationary aerial platform. In: AIAA LTA Systems Conference, Florida, p. 19 (2006)Google Scholar

Copyright information

© Springer Nature Switzerland AG 2019

Authors and Affiliations

  • Qunzhi Li
    • 1
  • Chao Ma
    • 2
    Email author
  • Wangjun Zhang
    • 1
  • Han Wang
    • 1
  • Zhihui Zhao
    • 1
  1. 1.Beijing Institute of Spacecraft System EngineeringBeijingChina
  2. 2.Beijing Key Laboratory of Intelligent Space Robotic Systems Technology and ApplicationsBeijing Institute of Spacecraft System EngineeringBeijingChina

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