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Publishing Language: Chinese

Prescribed performance sliding mode control for high-speed morphing vehicles based on high-order fully-actuated systems

Baisen WANG1,2,3Yiming LIAN1,2,3Peng WANG1,2,3( )
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
State Key Laboratory of High-Efficiency Reusable Aerospace Transportation Technology, Changsha 410073, China
Hunan Provincial Key Laboratory of Aerospace Cross-Domain Flight Vehicle Systems and Control Technology, Changsha 410073, China
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Abstract

To address the attitude control problem for High-speed Morphing Vehicles (HMVs) under strong coupling, parameter perturbations, and multi-source disturbances, this paper proposes a prescribed performance Super-Twisting Sliding Mode Control (STSMC) method based on High-Order Fully-Actuated Systems (HOFAS) modeling. Firstly, a high-order attitude dynamics model of the vehicle is established using the HOFAS approach. Through dynamic extension and variable elimination, the unmodeled dynamics induced by aerodynamic/structural coupling are mitigated, and the nonlinear dynamic equations are transformed into the HOFAS form. Through the parametric design for the characteristic polynomial coefficient matrix, the decoupling of state variables and separation of control are achieved. Secondly, to handle the lumped uncertainties arising from time-varying aerodynamic parameters during morphing and external disturbances, while also considering the dynamic response characteristics of the actuators, a super-twisting sliding mode controller based on Prescribed Performance Control (PPC) is designed. By constructing time-varying performance boundary functions, the controller robustly constrains attitude control errors and the asymptotic stability of the system is proven using a Lyapunov function. Finally, the performance of the proposed attitude controller is verified through Model-in-the-Loop (MIL) simulations and Hardware-in-the-Loop (HIL) experiments. The results demonstrate that the proposed method significantly reduces control chattering and validates its real-time performance and engineering practicability on an embedded platform.

CLC number: V488 Document code: A Article ID: 1000-6893(2026)11-332666-15

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
WANG B, LIAN Y, WANG P. Prescribed performance sliding mode control for high-speed morphing vehicles based on high-order fully-actuated systems. Acta Aeronautica et Astronautica Sinica, 2026, 47(11). https://doi.org/10.7527/S1000-6893.2025.32666

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Received: 11 August 2025
Revised: 04 September 2025
Accepted: 14 October 2025
Published: 20 October 2025
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica