SpringerLink
Log in

Adaptive Control Scheme for Carrier-Based UAVs with Actuator Failure

  • Conference paper
  • First Online:
Proceedings of 3rd 2023 International Conference on Autonomous Unmanned Systems (3rd ICAUS 2023) (ICAUS 2023)

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 1174))

Included in the following conference series:

  • 191 Accesses

Abstract

Considering the carrier landing task for a canard UAV, an adaptive control scheme is presented based on multivariable model reference adaptive control (MRAC) method. The UAV will suffer from external and internal disturbances during the landing process. The external disturbance includes the airwake and deck motion, while the internal disturbance denotes its own actuator failure. Simulation demonstrates that the proposed structure can improve tracking accuracy, rapidity, and robustness of glide path and attitude.

This work was supported by National Natural Science Foundation of China (61973158), Forward-Looking Layout of Scientific Research Projects of NUAA (1003-ILA22064), and Postgraduate Research & Practice Innovation Program of Jiangsu Province (KYCX21_0221).

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

Access this chapter

Log in via an institution

Subscribe and save

Springer+ Basic
EUR 32.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or Ebook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

Chapter
EUR 29.95
Price includes VAT (France)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
EUR 239.67
Price includes VAT (France)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Hardcover Book
EUR 295.39
Price includes VAT (France)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free ship** worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. Koo, S., Kim, S., Suk, J.: Model predictive control for UAV automatic landing on moving carrier deck with heave motion. IFAC-PapersOnLine 48(5), 59–64 (2015). https://doi.org/10.1016/j.ifacol.2015.06.464

    Article  Google Scholar 

  2. Zhen, Z., Tao, G., Yu, C., et al.: A multivariable adaptive control scheme for automatic carrier landing of UAV. Aerosp. Sci. Technol. 92, 714–721 (2019). https://doi.org/10.1016/j.ast.2019.06.030

    Article  Google Scholar 

  3. Yu, Y., Wang, H., Li, N., et al.: Automatic carrier landing system based on active disturbance rejection control with a novel parameters optimizer. Aerosp. Sci. Technol. 69, 149–160 (2017). https://doi.org/10.1016/j.ast.2017.06.026

    Article  Google Scholar 

  4. Lungu, M., Dinu, D.A., Chen, M., et al.: Inverse optimal control for autonomous carrier landing with disturbances. Aerosp. Sci. Technol. 139, 108382 (2023). https://doi.org/10.1016/j.ast.2023.108382

    Article  Google Scholar 

  5. Su, Z., Li, C., Zhen, Z.: Anti-disturbance constrained control of the air recovery carrier via an integral barrier Lyapunov function. Aerosp. Sci. Technol. 106, 106157 (2020). https://doi.org/10.1016/j.ast.2020.106157

    Article  Google Scholar 

  6. Yang, Z., Duan, H., Fan, Y., et al.: Automatic carrier landing system multilayer parameter design based on Cauchy mutation pigeon-inspired optimization. Aerosp. Sci. Technol. 79, 518–530 (2018). https://doi.org/10.1016/j.ast.2018.06.013

    Article  Google Scholar 

  7. Chang, J., Guo, Z., De, B.R., et al.: Predictor-based adaptive incremental nonlinear dynamic inversion for fault-tolerant flight control. IFAC-PapersOnLine 55(6), 730–736 (2022). https://doi.org/10.1016/j.ifacol.2022.07.214

    Article  Google Scholar 

  8. **ao, H., Zhen, Z., Xue, Y.: Fault-tolerant attitude tracking control for carrier-based aircraft using RBFNN-based adaptive second-order sliding mode control. Aerosp. Sci. Technol. 139, 108408 (2023). https://doi.org/10.1016/j.ast.2023.108408

    Article  Google Scholar 

  9. Wen, L., Tao, G., Yang, H., et al.: Adaptive actuator failure compensation for possibly nonminimum-phase systems using control separation based LQ design. IEEE Trans. Autom. Control 64(1), 143–158 (2018). https://doi.org/10.1109/TAC.2018.2809719

    Article  MathSciNet  Google Scholar 

  10. Li, B., Hu, Q., Yang, Y.: Continuous finite-time extended state observer based fault tolerant control for attitude stabilization. Aerosp. Sci. Technol. 84, 204–213 (2019). https://doi.org/10.1016/j.ast.2018.10.006

    Article  Google Scholar 

  11. Zhen, Z., Jiang, S., Ma, K.: Automatic carrier landing control for unmanned aerial vehicles based on preview control and particle filtering. Aerosp. Sci. Technol. 81, 99–107 (2018). https://doi.org/10.1016/j.ast.2018.07.039

    Article  Google Scholar 

  12. Li, Y., Liu, X., Ming, R., et al.: A cascaded nonlinear fault-tolerant control for fixed-wing aircraft with wing asymmetric damage. ISA Trans. 136, 503–524 (2023). https://doi.org/10.1016/j.isatra.2022.10.021

    Article  Google Scholar 

  13. Bolander, C.R., Hunsaker, D.F.: A sine-summation algorithm for the prediction of ship deck motion. In: OCEANS 2018 MTS/IEEE Charleston, pp. 1–10 (2018). https://doi.org/10.1109/OCEANS.2018.8604888

  14. Ngo, T.D., Sultan, C.: Model predictive control for helicopter shipboard operations in the ship airwakes. J. Guid. Control. Dyn. 39(3), 1–16 (2015). https://doi.org/10.2514/1.G001243

    Article  Google Scholar 

  15. Tao, G.: Adaptive Control Design and Analysis, pp. 149–C441. Wiley, New York (2003)

    Google Scholar 

  16. Gang, T.: Multivariable adaptive control: a survey. Automatica 50(11), 2737–2764 (2014). https://doi.org/10.1016/j.automatica.2014.10.015

    Article  MathSciNet  Google Scholar 

Download references

Author information

Authors and Affiliations

  1. State Key Laboratory of Mechanics and Control for Aerospace Structures, Nan**g University of Aeronautics and Astronautics, Nan**g, China

    Yixuan Xue, Yuchun Zou, Yikun Chen & Ziyang Zhen

  2. College of Automation Engineering, Nan**g University of Aeronautics and Astronautics, Nan**g, China

    Yixuan Xue, Yuchun Zou, Yikun Chen & Ziyang Zhen

Authors
  1. Yixuan Xue
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Yuchun Zou
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. Yikun Chen
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. Ziyang Zhen
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to Ziyang Zhen .

Editor information

Editors and Affiliations

  1. Nan**g University of Science and Technology, Nan**g, China

    Yi Qu

  2. Bei**g HIWING Scientific and Technological Information Institute, Bei**g, China

    Mancang Gu

  3. College of Intelligence Science and Technology, National University of Defense Technology, Changsha, Hunan, China

    Yifeng Niu

  4. Unmanned System Research Institute, Northwestern Polytechnical University, **'an, Shaanxi, China

    Wenxing Fu

Rights and permissions

Reprints and permissions

Copyright information

© 2024 Bei**g HIWING Scientific and Technological Information Institute

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

Xue, Y., Zou, Y., Chen, Y., Zhen, Z. (2024). Adaptive Control Scheme for Carrier-Based UAVs with Actuator Failure. In: Qu, Y., Gu, M., Niu, Y., Fu, W. (eds) Proceedings of 3rd 2023 International Conference on Autonomous Unmanned Systems (3rd ICAUS 2023). ICAUS 2023. Lecture Notes in Electrical Engineering, vol 1174. Springer, Singapore. https://doi.org/10.1007/978-981-97-1091-1_41

Download citation

Publish with us

Policies and ethics

Search

Navigation