Reinforcement Learning Control for Hypersonic Morphing Flight Vehicle with Identification of Dynamic Parameter

  • Conference paper
  • First Online:
Advances in Guidance, Navigation and Control ( ICGNC 2022)

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 845))

Included in the following conference series:

Abstract

A reinforcement learning (RL) controller with identification of the dynamic parameter of hypersonic morphing flight vehicle (HMFV) is proposed in this paper, successfully realizing the end-to-end control of attack angle in the longitudinal plane. The following improvements are made in this paper: Firstly, the dynamic parameter (rudder efficiency coefficient) of the flight vehicle is added into the state vector, so that the RL controller can understand the control ability of the rudder and generates the optimal control commands in the current state. Secondly, five instead of only one consecutive attack angle deviations are used to jointly generate the state vector, which enables the RL controller to use the model state information of the previous period of time and improve the control stability. Three simulations are set up in this paper. The simulation results show that the RL controller proposed in this paper can achieve stable and high precision attack angle control under large-scale environmental deviations and has strong generalization under different guidance commands.

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

Access this chapter

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 (Germany)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
EUR 459.03
Price includes VAT (Germany)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
EUR 588.49
Price includes VAT (Germany)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free ship** worldwide - see info
Hardcover Book
EUR 588.49
Price includes VAT (Germany)
  • 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

Similar content being viewed by others

References

  1. Liu, J.W., Gao, F., Luo, X.L.: Survey of deep reinforcement learning based on value function and policy gradient. Chin. J. Comput. (6), 1406–1438 (2019)

    Google Scholar 

  2. Zhen, Y., Yuan, J.Q., Chi, Q.X., Hao, M.R.: Research on application of deep reinforcement learning method in aircraft control. Tactical Missile Technol. (4), 112–118 (2020)

    Google Scholar 

  3. Zhang, Y.A., Ma, G.X., Liu, J.M., Sun, Y.M.: Reinforcement learning control modeling and algorithm design for the fixed wing UAV. Flight Dyn. (4), 88–96 (2019)

    Google Scholar 

  4. Li, R.F., Hu, L., Cai, L.: Adaptive tracking control of a hypersonic flight aircraft using neural networks with reinforcement synthesis. Aero Weaponry (6), 3–10 (2018)

    Google Scholar 

  5. Wang, G., Ma, C., Ru, H., Ma, G., **a, H.: An intelligent control method for non-affine hypersonic vehicle. Flight Control Detect. (4), 59–65 (2021)

    Google Scholar 

  6. Zhang, Z.B., Li, X.H., An, J.P., Man, W.X., Zhang, G.H.: Model-free attitude control of spacecraft based on PID-guide TD3 algorithm. Int. J. Aerosp. Eng. 1–13 (2020)

    Google Scholar 

  7. Shen, Y., Chen, M.: Reinforcement learning based dynamic inverse attitude control of near-space vehicle. In: 2020 39th Chinese Control Conference (CCC), pp. 6972–6977 (2020)

    Google Scholar 

  8. Huang, X., Liu, J.R., Jia, C.H., et al.: Deep deterministic policy gradient algorithm for UAV control. Acta Aeronautica et Astronautica Sinica42(11), 524688 (2021). (in Chinese). https://doi.org/10.7527/S10006-893.2020.24688

  9. Zhang, Z.N., Zhang, R., Nie, W.M., et al.: Adaptive optimal attitude control of reentry vehicles. J. Astronaut. (2), 199–206 (2019)

    Google Scholar 

  10. Nie, Y., Yu, C.M., Bai, W.Y.: Aircraft dynamic parameter identification based on adaptive weight Kalman filter. In: 2021 The China Automation Congress (CAC) (2021)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Chunmei Yu .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2023 The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

Nie, Y., Zhang, Y., Bai, W., Cao, Y., Yu, C. (2023). Reinforcement Learning Control for Hypersonic Morphing Flight Vehicle with Identification of Dynamic Parameter. In: Yan, L., Duan, H., Deng, Y. (eds) Advances in Guidance, Navigation and Control. ICGNC 2022. Lecture Notes in Electrical Engineering, vol 845. Springer, Singapore. https://doi.org/10.1007/978-981-19-6613-2_250

Download citation

Publish with us

Policies and ethics

Navigation