Skip to main content
Log in

On the sub-low contact velocity control of rendezvous docking for smart world

  • Published:
Cluster Computing Aims and scope Submit manuscript

Abstract

In order to avoid damages caused by high-speed collision during the rendezvous and docking process, the contact velocity between two spacecrafts has to be as low as possible. But in practice, it is very difficult to find the minimum value of contact velocity because of the complicated function involved. The only method to find the minimum of a function is by differentiating. However, this method is used to solve the problem of minimum speed, which is not only complicated in operation but also difficult to eliminate in the local minimum. Moreover, space applications should also consider the limitation of operation speed. For this reason, this paper proposes a method to find the sub-low relative speed, and derives the control law of rendezvous and docking.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3

Similar content being viewed by others

References

  1. Liang, J., Ma, O.: Angular velocity tracking for satellite rendezvous and docking. Acta Astronaut. 69(11–12), 1019–1028 (2011)

    Google Scholar 

  2. Diao, X, Liang, J., Ma, O.: Angular-velocity tracking with unknown dynamics for satellite rendezvous and docking. In: Proceedings of SPIE—The International Society for Optical Engineering, p. 7330 (2009)

  3. Singla, P., Subbarao, K., Junkins, J.L.: Adaptive output feedback control for spacecraft rendezvous and docking under measurement uncertainty. J. Guidance Control Dyn. 29(4), 892–902 (2012)

    Google Scholar 

  4. Nicolai, A., Raschke, C., Stoltz, S., et al.: The attitude control system of a rendezvous and docking technology demonstrator mission target. In: Aerospace Conference, pp. 1–12. IEEE (2015)

  5. Yu, F., He, Z.: The coupled and decoupled relative navigation algorithms for rendezvous and docking of a malfunctioned spacecraft. In: Control Conference, pp. 5374–5379. IEEE (2016)

  6. Kemble, S.: Automated rendezvous and docking of spacecraft [J]. Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. 221(6), 997 (2007)

    Google Scholar 

  7. Evdokimov, S.N., Klimanov, S.I., Komarova, L.I., et al.: Control of angular motion of a landing module of “Soyuz” type upon satellite returning from the orbit. J. Comput. Syst. Sci. Int. 50(5), 826–836 (2011)

    Google Scholar 

  8. Roe, F., Betts, K., Carrington, C.: Hydra rendezvous and docking sensor system. In: Aerospace Conference, pp. 1–10. IEEE (2007)

  9. Upadhyay, T., Cotterill, S., Deaton, A.: Autonomous reconfigurable GPS/INS navigation and pointing system forrendezvous and docking. In: Automated Rendezvous and Capture Review. Executive Summary. Automated Rendezvous and Capture Review. Executive Summary (2013)

  10. Bryan, T., Roe, F., Coker, C.: Automated rendezvous and capture development infrastructure. Automated Rendezvous and Capture Review. Executive Summary Automated Rendezvous and Capture Review. Executive Summary, pp. 263–271 (2013)

Download references

Acknowledgements

This paper is supported by Shanxi Nature Science Foundation (Grant No. 2015011040).The authors would like to express thanks for the anonymous reviewers’ and the editors’ instructive suggestions which to a great degree improved the quality of this paper.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Jianguo Ju.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Xing, J., Ju, J. On the sub-low contact velocity control of rendezvous docking for smart world. Cluster Comput 22 (Suppl 2), 3123–3130 (2019). https://doi.org/10.1007/s10586-018-1984-7

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10586-018-1984-7

Keywords

Navigation