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ADRC-Based Attitude Control Laws Design for Morphing Aircraft

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Advances in Guidance, Navigation and Control ( ICGNC 2022)

Abstract

Aerodynamic parameters change when morphing aircraft performs the morphing process, thereby varying the aerodynamic characteristics of the aircraft. Flying stability and control accuracy may not be guaranteed by common methods. Taking the variable-sweep aircraft as research object, aiming at the uncertainty problems of nonlinear model of morphing aircraft in morphing process, this paper designs triaxial attitude control laws based on active disturbance rejection control (ADRC). The changes of aerodynamic characteristics while morphing and the strong coupling between different channels are treated as disturbances, and included in total disturbance of the whole system, which is cancelled by the means of extended state observer (ESO). The simulation result indicates that the proposed attitude control laws show great control effect for varying sweeps, with high control precision and strong robustness.

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References

  1. Zhang, Y.B., Liu, M.D., Xiong, J.J.: Morphing aircraft technology. Aeronaut. Sci. Technol. 6, 64–68 (2013)

    Google Scholar 

  2. Lee, J., et al.: Linear parameter-varying control of variable span-sweep morphing aircraft. In: AIAA SciTech Forum, AIAA, p. 0106 (2019)

    Google Scholar 

  3. Wu, Q., et al.: Design of sliding mode controller with self-adaption for a morphing aircraft. In: Proceedings of the 2018 Chinese Automation Congress, pp. 122–127. IEEE (2018)

    Google Scholar 

  4. Qiao, F., et al.: A high precision adaptive back-stepping control method for morphing aircraft based on RBFNN method. J. Northwestern Polytech. Uni. 38(3), 540–549 (2020)

    Article  MathSciNet  Google Scholar 

  5. Jie, Z.: H∞ robust adaptive controller for a morphing aircraft based on SRAD and LPV model. In: Proceedings of the 2018 Chinese Control and Decision Conference, pp. 5250–5255. IEEE (2018)

    Google Scholar 

  6. Han, J.: active disturbance rejection controller and application. Control Decis. 13(1), 19–23 (1998)

    Google Scholar 

  7. Zhao, S., Gao, Z.: Active Disturbance Rejection Control for Non-minimum Phase Systems. In: Proceedings of the 29th Chinese Control Conference, IEEE, pp. 6066–6070 (2010)

    Google Scholar 

  8. Zhao, S., Gao, Z.: Modified active disturbance rejection control for time-delay systems. ISA Trans. 53, 882–888 (2014)

    Article  Google Scholar 

  9. Zheng, Q., Gao, Z.: On active disturbance rejection for systems with input time-delays and unknown dynamics. In: Proceedings of the 2016 American Control Conference, pp. 95–100. IEEE (2016)

    Google Scholar 

  10. Wang, H., et al.: Active disturbance rejection control for discrete systems with zero dynamics. Int. J. Robust Nonlinear Control 31, 5298–5311 (2021)

    Article  MathSciNet  Google Scholar 

  11. RamírezNeria, M., et al.: Active disturbance rejection control for reference trajectory tracking tasks in the Pendubot system. IEEE Access 9, 102663–102670 (2021)

    Article  Google Scholar 

  12. Seigler, T.M., et al.: Modeling and flight control of large-scale morphing aircraft. J. Aircr. 44(4), 1077–1087 (2007)

    Article  Google Scholar 

  13. Seigler, T.M., Neal, D.A.: Analysis of transition stability for morphing aircraft. J. Guid. Control Dyn. 32(6), 1947–1954 (2009)

    Article  Google Scholar 

  14. Han, J.: From PID to active disturbance rejection control. IEEE Trans. Ind. Electron. 56(3), 900–906 (2009)

    Article  Google Scholar 

Download references

Acknowledgement

This research is supported by the National Natural Science Foundation of China (No. 62073266), the Aeronautical Science Foundation of China (No. 201905053003), and the Key Laboratory of flight control simulation technology of China.

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Correspondence to Xiaoxiong Liu .

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Li, K., Liu, X., Li, Y. (2023). ADRC-Based Attitude Control Laws Design for Morphing Aircraft. 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_496

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