Skip to main content
Log in

Target selection and transfer trajectories design for exploring asteroid mission

  • Published:
Science China Technological Sciences Aims and scope Submit manuscript

Abstract

Technique of target selection and profiles of transfer trajectory for Chinese asteroid exploring mission are studied systemically. A complete set of approaches to selecting mission targets and designing the transfer trajectory is proposed. First, when selecting a target for mission, some factors regarded as the scientific motivations are discussed. Then, when analyzing the accessibility of targets, instead of the classical strategy, the multiple gravity-assist strategy is provided. The suitable and possible targets, taking into account scientific value and technically feasible, are obtained via selection and estimation. When designing the transfer trajectory for exploring asteroid mission, an approach to selecting gravity-assist celestial body is proposed. Finally, according to the mission constraints, the trajectory profile with 2-years ΔV-EGA for exploring asteroid is presented. Through analyzing the trajectory profile, unexpected result that the trajectory would pass by two main-belts asteroids is found. So, the original proposal is extended to the multiple flybys mission. It adds the scientific return for asteroid mission.

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.

Similar content being viewed by others

References

  1. Hulkower N D, Lau C O, Bender D F. Optimum two-impulse transfer for preliminary interplanetary trajectory design. J Guid Control Dyn, 1984, 7: 458–461

    Article  Google Scholar 

  2. Lau C O, Hulkower N D. Accessibility of Near-Earth asteroids. J Guid Control Dyn, 1987, 10: 225–232

    Article  Google Scholar 

  3. Perozzi E, Rossi A, Valsecchi G B. Basic targeting strategies for rendezvous and flyby missions to the Near-Earth asteroids. Planet Space Sci, 2001, 49: 3–22

    Article  Google Scholar 

  4. Binzel R P, Perozzi E, Rivkin A S, et al. Dynamical and compositional assessment of Near-Earth object mission targets. Meteoritics Planet Sci, 2004, 39: 351–366

    Article  Google Scholar 

  5. Qiao D, Cui H T, Cui P Y. Evaluating accessibility of Near-Earth asteroids via Earth gravity assists. J Guid, Control Dyn, 2006, 29: 502–505

    Article  Google Scholar 

  6. Qiao D, Cui H T, Cui P Y. Design and analyze optimum two-impulse transfer trajectory for exploring asteroids (in Chinese). J Astronaut, 2005, 26: 362–367

    Google Scholar 

  7. Longuski J M, Williams S N. Automated design of gravity-assist trajectories to Mars and the outer planets. Celes Mech Dyn Astron, 1991, 52: 207–220

    Article  Google Scholar 

  8. Bonfiglio E P, Longuski J M. Automated design of aerogravity-assist trajectories. J Spac Rock, 2000, 37: 768–775

    Article  Google Scholar 

  9. Sims J A, Longuski J M, Staugler A J. V Leveraging for inter planetary missions: multiple-revolution orbit techniques. J Guid Control Dyn, 1997, 20: 409–415

    Article  MATH  Google Scholar 

  10. Guo H L, Wang Z S, Qu G J. Flight theory and analysis of launch opportunity for Mars explosion (in Chinese). Sci China Ser E-Tech Sci, 2009, 39: 535–543

    Google Scholar 

  11. Lorenzo C, Guido C, Dario P. Optimization procedure for preliminary design of opposition-class Mars mission. J Guid Control Dyn, 1998, 21: 134–140

    Article  MATH  Google Scholar 

  12. Qiao D, Cui H T, Cui P Y. The design of transfer trajectory for Ivar asteroid exploration. Acta Astronaut, 2009, 65: 1553–1560

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to PingYuan Cui.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Cui, P., Qiao, D., Cui, H. et al. Target selection and transfer trajectories design for exploring asteroid mission. Sci. China Technol. Sci. 53, 1150–1158 (2010). https://doi.org/10.1007/s11431-010-0007-6

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11431-010-0007-6

Keywords

Navigation