Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control

Heting Wang; Hui Wang; Keqing Guo; Daoguang Tang; Yuanyue Lei

doi:10.23919/CCC58697.2023.10241223

Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control

Heting Wang, Hui Wang, Keqing Guo, Daoguang Tang^*, Yuanyue Lei

^*Corresponding author for this work

School of Aerospace Engineering

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

Abstract

The lateral linear control model of missile is established and the symbol definition of lateral aerodynamic transfer function is given in this paper. And the frequency domain characteristics of the lateral airframe are analyzed in the low, middle and high frequency band, respectively. Combined with the active disturbance rejection control method, a lateral three-loop autopilot based on linear active disturbance rejection control is proposed. Through the dynamic estimation and compensation of the extended state observer, the robustness to the system uncertainty is enhanced. Simulation results of different cases demonstrate the effectiveness and robustness of proposed autopilots and lateral active disturbance rejection three-loop autopilot is more robust.

Original language	English
Title of host publication	2023 42nd Chinese Control Conference, CCC 2023
Publisher	IEEE Computer Society
Pages	3552-3558
Number of pages	7
ISBN (Electronic)	9789887581543
DOIs	https://doi.org/10.23919/CCC58697.2023.10241223
Publication status	Published - 2023
Event	42nd Chinese Control Conference, CCC 2023 - Tianjin, China Duration: 24 Jul 2023 → 26 Jul 2023

Publication series

Name	Chinese Control Conference, CCC
Volume	2023-July
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	42nd Chinese Control Conference, CCC 2023
Country/Territory	China
City	Tianjin
Period	24/07/23 → 26/07/23

Keywords

Active disturbance rejection
Lateral autopilot
Missile lateral dynamics
Pseudo-angle of sideslip

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10.23919/CCC58697.2023.10241223

Cite this

Wang, H., Wang, H., Guo, K., Tang, D., & Lei, Y. (2023). Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control. In 2023 42nd Chinese Control Conference, CCC 2023 (pp. 3552-3558). (Chinese Control Conference, CCC; Vol. 2023-July). IEEE Computer Society. https://doi.org/10.23919/CCC58697.2023.10241223

@inproceedings{6aa299c5828a41fc84a0f28089a6cbd5,

title = "Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control",

abstract = "The lateral linear control model of missile is established and the symbol definition of lateral aerodynamic transfer function is given in this paper. And the frequency domain characteristics of the lateral airframe are analyzed in the low, middle and high frequency band, respectively. Combined with the active disturbance rejection control method, a lateral three-loop autopilot based on linear active disturbance rejection control is proposed. Through the dynamic estimation and compensation of the extended state observer, the robustness to the system uncertainty is enhanced. Simulation results of different cases demonstrate the effectiveness and robustness of proposed autopilots and lateral active disturbance rejection three-loop autopilot is more robust.",

keywords = "Active disturbance rejection, Lateral autopilot, Missile lateral dynamics, Pseudo-angle of sideslip",

author = "Heting Wang and Hui Wang and Keqing Guo and Daoguang Tang and Yuanyue Lei",

note = "Publisher Copyright: {\textcopyright} 2023 Technical Committee on Control Theory, Chinese Association of Automation.; 42nd Chinese Control Conference, CCC 2023 ; Conference date: 24-07-2023 Through 26-07-2023",

year = "2023",

doi = "10.23919/CCC58697.2023.10241223",

language = "English",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "3552--3558",

booktitle = "2023 42nd Chinese Control Conference, CCC 2023",

address = "United States",

}

Wang, H, Wang, H, Guo, K, Tang, D & Lei, Y 2023, Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control. in 2023 42nd Chinese Control Conference, CCC 2023. Chinese Control Conference, CCC, vol. 2023-July, IEEE Computer Society, pp. 3552-3558, 42nd Chinese Control Conference, CCC 2023, Tianjin, China, 24/07/23. https://doi.org/10.23919/CCC58697.2023.10241223

Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control. / Wang, Heting; Wang, Hui; Guo, Keqing et al.
2023 42nd Chinese Control Conference, CCC 2023. IEEE Computer Society, 2023. p. 3552-3558 (Chinese Control Conference, CCC; Vol. 2023-July).

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

TY - GEN

T1 - Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control

AU - Wang, Heting

AU - Wang, Hui

AU - Guo, Keqing

AU - Tang, Daoguang

AU - Lei, Yuanyue

PY - 2023

Y1 - 2023

N2 - The lateral linear control model of missile is established and the symbol definition of lateral aerodynamic transfer function is given in this paper. And the frequency domain characteristics of the lateral airframe are analyzed in the low, middle and high frequency band, respectively. Combined with the active disturbance rejection control method, a lateral three-loop autopilot based on linear active disturbance rejection control is proposed. Through the dynamic estimation and compensation of the extended state observer, the robustness to the system uncertainty is enhanced. Simulation results of different cases demonstrate the effectiveness and robustness of proposed autopilots and lateral active disturbance rejection three-loop autopilot is more robust.

AB - The lateral linear control model of missile is established and the symbol definition of lateral aerodynamic transfer function is given in this paper. And the frequency domain characteristics of the lateral airframe are analyzed in the low, middle and high frequency band, respectively. Combined with the active disturbance rejection control method, a lateral three-loop autopilot based on linear active disturbance rejection control is proposed. Through the dynamic estimation and compensation of the extended state observer, the robustness to the system uncertainty is enhanced. Simulation results of different cases demonstrate the effectiveness and robustness of proposed autopilots and lateral active disturbance rejection three-loop autopilot is more robust.

KW - Active disturbance rejection

KW - Lateral autopilot

KW - Missile lateral dynamics

KW - Pseudo-angle of sideslip

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U2 - 10.23919/CCC58697.2023.10241223

DO - 10.23919/CCC58697.2023.10241223

M3 - Conference contribution

AN - SCOPUS:85175539875

T3 - Chinese Control Conference, CCC

SP - 3552

EP - 3558

BT - 2023 42nd Chinese Control Conference, CCC 2023

PB - IEEE Computer Society

T2 - 42nd Chinese Control Conference, CCC 2023

Y2 - 24 July 2023 through 26 July 2023

ER -

Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control

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