Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer

Yizheng Li; Junhui Liu; Jiayuan Shan; Chunyan Wang; Yadong Chen

doi:10.1007/978-981-19-6613-2_622

Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer

Yizheng Li, Junhui Liu^*, Jiayuan Shan, Chunyan Wang, Yadong Chen

^*Corresponding author for this work

School of Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

1 Citation (Scopus)

Abstract

In this paper, a linear parameter-varying (LPV) controller with extended state observer (ESO) is designed to reject the disturbance of morphing aircraft during shape varying. Considering additional forces and moments due to transition process of morphing, the longitudinal nonlinear mathematical model of variable span-sweep morphing aircraft is established. After transforming the nonlinear model into affine LPV system, the gain scheduling controller is designed. Therefore, the flight stability of morphing aircraft is guaranteed during the shape varying process. To compensate the disturbances caused by additional forces, moment and aerodynamic uncertainties, an ESO is applied to estimate the system states and disturbances of morphing aircraft. Finally, the effectiveness of proposed controller is validated through numerical simulations.

Original language	English
Title of host publication	Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
Editors	Liang Yan, Haibin Duan, Yimin Deng, Liang Yan
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	6450-6459
Number of pages	10
ISBN (Print)	9789811966125
DOIs	https://doi.org/10.1007/978-981-19-6613-2_622
Publication status	Published - 2023
Event	International Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, China Duration: 5 Aug 2022 → 7 Aug 2022

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	845 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	International Conference on Guidance, Navigation and Control, ICGNC 2022
Country/Territory	China
City	Harbin
Period	5/08/22 → 7/08/22

Keywords

Extended state observer
Linear parameter-varying
Morphing aircraft
Variable span-sweep

Access to Document

10.1007/978-981-19-6613-2_622

Cite this

Li, Y., Liu, J., Shan, J., Wang, C., & Chen, Y. (2023). Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer. In L. Yan, H. Duan, Y. Deng, & L. Yan (Eds.), Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control (pp. 6450-6459). (Lecture Notes in Electrical Engineering; Vol. 845 LNEE). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-19-6613-2_622

Li, Yizheng ; Liu, Junhui ; Shan, Jiayuan et al. / Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer. Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. editor / Liang Yan ; Haibin Duan ; Yimin Deng ; Liang Yan. Springer Science and Business Media Deutschland GmbH, 2023. pp. 6450-6459 (Lecture Notes in Electrical Engineering).

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title = "Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer",

abstract = "In this paper, a linear parameter-varying (LPV) controller with extended state observer (ESO) is designed to reject the disturbance of morphing aircraft during shape varying. Considering additional forces and moments due to transition process of morphing, the longitudinal nonlinear mathematical model of variable span-sweep morphing aircraft is established. After transforming the nonlinear model into affine LPV system, the gain scheduling controller is designed. Therefore, the flight stability of morphing aircraft is guaranteed during the shape varying process. To compensate the disturbances caused by additional forces, moment and aerodynamic uncertainties, an ESO is applied to estimate the system states and disturbances of morphing aircraft. Finally, the effectiveness of proposed controller is validated through numerical simulations.",

keywords = "Extended state observer, Linear parameter-varying, Morphing aircraft, Variable span-sweep",

author = "Yizheng Li and Junhui Liu and Jiayuan Shan and Chunyan Wang and Yadong Chen",

note = "Publisher Copyright: {\textcopyright} 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.; International Conference on Guidance, Navigation and Control, ICGNC 2022 ; Conference date: 05-08-2022 Through 07-08-2022",

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Li, Y, Liu, J , Shan, J , Wang, C & Chen, Y 2023, Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer. in L Yan, H Duan, Y Deng & L Yan (eds), Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. Lecture Notes in Electrical Engineering, vol. 845 LNEE, Springer Science and Business Media Deutschland GmbH, pp. 6450-6459, International Conference on Guidance, Navigation and Control, ICGNC 2022, Harbin, China, 5/08/22. https://doi.org/10.1007/978-981-19-6613-2_622

Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer. / Li, Yizheng; Liu, Junhui ; Shan, Jiayuan et al.
Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. ed. / Liang Yan; Haibin Duan; Yimin Deng; Liang Yan. Springer Science and Business Media Deutschland GmbH, 2023. p. 6450-6459 (Lecture Notes in Electrical Engineering; Vol. 845 LNEE).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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N2 - In this paper, a linear parameter-varying (LPV) controller with extended state observer (ESO) is designed to reject the disturbance of morphing aircraft during shape varying. Considering additional forces and moments due to transition process of morphing, the longitudinal nonlinear mathematical model of variable span-sweep morphing aircraft is established. After transforming the nonlinear model into affine LPV system, the gain scheduling controller is designed. Therefore, the flight stability of morphing aircraft is guaranteed during the shape varying process. To compensate the disturbances caused by additional forces, moment and aerodynamic uncertainties, an ESO is applied to estimate the system states and disturbances of morphing aircraft. Finally, the effectiveness of proposed controller is validated through numerical simulations.

AB - In this paper, a linear parameter-varying (LPV) controller with extended state observer (ESO) is designed to reject the disturbance of morphing aircraft during shape varying. Considering additional forces and moments due to transition process of morphing, the longitudinal nonlinear mathematical model of variable span-sweep morphing aircraft is established. After transforming the nonlinear model into affine LPV system, the gain scheduling controller is designed. Therefore, the flight stability of morphing aircraft is guaranteed during the shape varying process. To compensate the disturbances caused by additional forces, moment and aerodynamic uncertainties, an ESO is applied to estimate the system states and disturbances of morphing aircraft. Finally, the effectiveness of proposed controller is validated through numerical simulations.

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Li Y, Liu J , Shan J , Wang C, Chen Y. Disturbance Rejection LPV Control of Morphing Aircraft Based on Extended State Observer. In Yan L, Duan H, Deng Y, Yan L, editors, Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. Springer Science and Business Media Deutschland GmbH. 2023. p. 6450-6459. (Lecture Notes in Electrical Engineering). doi: 10.1007/978-981-19-6613-2_622