TY - GEN
T1 - Active Disturbance Rejection Control of Telescopic-Wing Morphing Aircraft
T2 - 17th International Conference on Intelligent Robotics and Applications, ICIRA 2024
AU - Wang, Haoyu
AU - Pang, Muyao
AU - Wang, Zhaolei
AU - Cao, Fangfei
N1 - Publisher Copyright:
© The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.
PY - 2025
Y1 - 2025
N2 - Compared to fixed-wing aircraft, telescopic-wing morphing aircraft can improve aerodynamic characteristics and adapt to variable flight environments through the extension and retraction of their wings. However, the control system of a telescopic-wing aircraft is complex and must handle a wide range of operating conditions. Its configuration exhibits typical linear parameter-varying (LPV) characteristics as it changes with the environment and operating conditions, presenting a significant challenge to control algorithms. This paper addresses the model's parameter-varying features and uncertainties during the deformation process of the telescopic wing aircraft, as well as external multi-source disturbances, by designing an Active Disturbance Rejection Control (ADRC) algorithm. Software simulation studies were conducted on the established model and the designed algorithm using the MATLAB/Simulink platform, achieving stable control of the telescopic wing aircraft's deformation flight process and effectively suppressing composite disturbances. Additionally, a sliding mode gain-scheduled control strategy was employed to control the aircraft's deformation flight process, serving as a comparison to the ADRC, thereby verifying the superiority of the ADRC method.
AB - Compared to fixed-wing aircraft, telescopic-wing morphing aircraft can improve aerodynamic characteristics and adapt to variable flight environments through the extension and retraction of their wings. However, the control system of a telescopic-wing aircraft is complex and must handle a wide range of operating conditions. Its configuration exhibits typical linear parameter-varying (LPV) characteristics as it changes with the environment and operating conditions, presenting a significant challenge to control algorithms. This paper addresses the model's parameter-varying features and uncertainties during the deformation process of the telescopic wing aircraft, as well as external multi-source disturbances, by designing an Active Disturbance Rejection Control (ADRC) algorithm. Software simulation studies were conducted on the established model and the designed algorithm using the MATLAB/Simulink platform, achieving stable control of the telescopic wing aircraft's deformation flight process and effectively suppressing composite disturbances. Additionally, a sliding mode gain-scheduled control strategy was employed to control the aircraft's deformation flight process, serving as a comparison to the ADRC, thereby verifying the superiority of the ADRC method.
KW - ADRC
KW - LPV
KW - Morphing aircraft
KW - Telescopic-wing aircraft
UR - http://www.scopus.com/inward/record.url?scp=85218447104&partnerID=8YFLogxK
U2 - 10.1007/978-981-96-0789-1_31
DO - 10.1007/978-981-96-0789-1_31
M3 - Conference contribution
AN - SCOPUS:85218447104
SN - 9789819607884
T3 - Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
SP - 424
EP - 437
BT - Intelligent Robotics and Applications - 17th International Conference, ICIRA 2024, Proceedings
A2 - Lan, Xuguang
A2 - Mei, Xuesong
A2 - Jiang, Caigui
A2 - Zhao, Fei
A2 - Tian, Zhiqiang
PB - Springer Science and Business Media Deutschland GmbH
Y2 - 31 July 2024 through 2 August 2024
ER -