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Spacecraft rendezvous trajectory safety quantitative performance index eliminating probability dilution

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Abstract

In view of the probability dilution problem of the existing quantitative indexes of rendezvous trajectory safety performance using collision probability, this paper proposes a new quantitative index of rendezvous trajectory safety performance by well combining collision probability with warning threshold. The proposed new index increases monotonously as the position errors of the chaser spacecraft increase, therefore it can effectively overcome the problems of the reduction in the largest performance value and the advancement in the most dangerous time induced by the probability dilution. The proposed new index is applied to the safety design of close range rendezvous missions. The mission’s safety requirements for initial navigation precision and the safe region of initial and final keeping points’ positions with a certain navigation precision are analyzed, and several valuable conclusions about the relation between position navigation precision and velocity navigation precision as well as the relation between keeping points’ positions and navigation precision are obtained.

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References

  1. Fehse W. Automated Rendezvous and Docking of Spacecraft. London: Cambridge University Press, 2003. 76–111

    Book  Google Scholar 

  2. Tang G J, Luo Y Z, Zhang J. Mission Plan of Rendezvous and Docking (in Chinese). Beijing: Science Press, 2008. 232–249

    Google Scholar 

  3. Luo Y Z, Zhang J, Tang G J. Survey of orbital dynamics and control of space rendezvous. Chin J Aeronaut, 2014, 27:1–11

    Article  Google Scholar 

  4. Li H N, Gao Z Z, Li J S, et al. Mathematical prototypes for collocating geostationary satellites. Sci China Tech Sci, 2013, 56: 1086–1092

    Article  Google Scholar 

  5. Wu W R, Liu W W, Qiao D, et al. Investigation on the development of deep space exploration. Sci China Tech Sci, 2012, 55: 1086–1091

    Article  Google Scholar 

  6. Kawano I, Mokuno M, Kasai T, et al. Result of autonomous rendezvous docking experiment of engineering test satellite-VII. J Spacecr Rockets, 2001, 38: 105–111

    Article  Google Scholar 

  7. Croomes S. Overview of the DART Mishap Investigation Results. NASA Report, 2006

    Google Scholar 

  8. Zhu R Z, Tang Y, Yin Y. Safety mode design of final translation trajectories of space rendezvous (in Chinese). J Astronaut, 2004, 25: 443–448

    Google Scholar 

  9. Xie Y C, Chen C Q. Safe retreat trajectory design for rendezvous behind a keep-out zone (in Chinese). Aerosp Control Appl, 2009, 35: 1–5

    Google Scholar 

  10. Ma L, Meng X, Liu Z, et al. Suboptimal power-limited rendezvous with fixed docking direction and collision avoidance. J Guid Control Dynam, 2013, 36: 229–239

    Article  Google Scholar 

  11. Luo Y Z, Tang G J, Lei Y J. Optimal multi-objective linearized rendezvous. J Guid Control Dynam, 2007, 30: 383–389

    Article  Google Scholar 

  12. Breger L, How J P. Safe trajectories for autonomous rendezvous of spacecraft. J Guid Control Dynam, 2008, 31: 1478–1489

    Article  Google Scholar 

  13. Woodburn J, Tanygin S. Position covariance visualization. In: AIAA/AAS Astrodynamics Specialist Conference and Exhibit. Monterey, California: AIAA 2002-4985, 2002

    Google Scholar 

  14. Liang L B, Luo Y Z, Wang H, et al. Study on the quantitative performance index of space rendezvous trajectory safety (in Chinese). J Astronaut, 2010, 31: 2239–2244

    Google Scholar 

  15. Luo Y Z, Liang L B, Wang H, et al. Quantitative performance for spacecraft rendezvous trajectory safety. J Guid Control Dynam, 2011, 34: 1264–1269

    Article  Google Scholar 

  16. Niu Z Y. Safety Assessment Method and Design Optimization of Rendezvous Trajectory in View of Early Warning Threshold (in Chinese). Dissertation for Master’s Degree. Changsha: National University of Defense Technology, 2012. 27–39

    Google Scholar 

  17. Alfano S. Relating position uncertainty to maximum conjunction probability. In: AAS/AIAA Astrodynamics Specialists Conference. Big Sky, Montana: AAS 03-548, 2003

    Google Scholar 

  18. Peterson G E. NEO orbit uncertainties and their effect on risk assessment. In: 2004 Planetary Defense Conference: Protecting Earth from Asteroids. Orange County, California: AIAA 2004-1420, 2004

    Google Scholar 

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Correspondence to YaZhong Luo.

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Sun, Z., Luo, Y. & Niu, Z. Spacecraft rendezvous trajectory safety quantitative performance index eliminating probability dilution. Sci. China Technol. Sci. 57, 1219–1228 (2014). https://doi.org/10.1007/s11431-014-5523-3

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  • DOI: https://doi.org/10.1007/s11431-014-5523-3

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