Skip to main content
Log in

Robust transition trajectory optimization for tail-sitter UAVs considering uncertainties

  • Letter
  • Published:
Science China Information Sciences Aims and scope Submit manuscript

Conclusion

In this study, the robust transition trajectory optimization was conducted for tail-sitter UAVs. The correlated stochastic uncertainties are different from existing deterministic optimal transition studies and are considered for the first time. Simulation results show that the robustness of the derived transition trajectories is improved. In the future, we will study more complicated unknown uncertainties. In addition, the robust control law for the tail-sitter transition phases will also be studied.

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

Access this article

Subscribe and save

Springer+ Basic
$34.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or eBook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

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

Instant access to the full article PDF.

References

  1. Wang K L, Ke Y J, Chen B M. Autonomous reconfigurable hybrid tail-sitter UAV U-Lion. Sci China Inf Sci, 2017, 60: 033201

    Article  Google Scholar 

  2. Bai T T, Wang D B. Cooperative trajectory optimization for unmanned aerial vehicles in a combat environment. Sci China Inf Sci, 2019, 62: 010205

    Article  Google Scholar 

  3. Banazadeh A, Taymourtash N. Optimal control of an aerial tail sitter in transition flight phases. J Aircraft, 2016, 53: 914–921

    Article  Google Scholar 

  4. Naldi R, Marconi L. Optimal transition maneuvers for a class of V/STOL aircraft. Automatica, 2011, 47: 870–879

    Article  MathSciNet  Google Scholar 

  5. Maqsood A, Go T H. Optimization of Hover-to-Cruise transition maneuver using variable-incidence wing. J Aircraft, 2010, 47: 1060–1064

    Article  Google Scholar 

  6. Yang Y J, Wang X Y, Zhu J H, et al. Dynamic transition corridors and control strategy of a rotor-blown-wing tail-sitter. J Guid Control Dyn, 2021, 44: 1836–1852

    Article  Google Scholar 

  7. Xiu D, Karniadakis G E. The Wiener-Askey polynomial chaos for stochastic differential equations. SIAM J Sci Comput, 2002, 24: 619–644

    Article  MathSciNet  Google Scholar 

  8. Eldred M, Webster C, Constantine P. Evaluation of nonintrusive approaches for Wiener-Askey generalized polynomial chaos. In: Proceedings of the 49th AIAA/ASME Structures, Structural Dynamics, and Materials Conference, Schaumburg, 2008. 1892

  9. Agrawal S K, Fabien B C. Optimization of Dynamic Systems. New York: Springer Science & Business Media, 2013. 93–108

    Google Scholar 

Download references

Acknowledgements

This work was supported by National Natural Science Foundation of China (Grant Nos. 62073185, 61903216, 61973182).

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Xiangyang Wang.

Additional information

Supporting information

Appendixes A–D. The supporting information is available online at info.scichina.com and link.springer.com. The supporting materials are published as submitted, without typesetting or editing. The responsibility for scientific accuracy and content remains entirely with the authors.

Supplementary File

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Yang, Y., Wang, X., Zhu, J. et al. Robust transition trajectory optimization for tail-sitter UAVs considering uncertainties. Sci. China Inf. Sci. 66, 169201 (2023). https://doi.org/10.1007/s11432-020-3257-x

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • DOI: https://doi.org/10.1007/s11432-020-3257-x