The design of predefined-time anti-saturation attitude control with disturbance observer for hypersonic morphing vehicles

Abstract This paper addresses the attitude control challenge of hypersonic morphing vehicles (HMVs) with uncertainties and actuator saturation. The primary contribution of this work lies in achieving a predefined settling time while ensuring robust control performance under morphing effects, actuator saturation and disturbances. Firstly, a control-oriented model is established based on the dynamics of HMVs. Subsequently, a nonsingular multivariable sliding mode manifold, utilising a switching function, is designed to attain predefined-time convergence and prevent singularity issues. A disturbance observer with an adaptive law is developed to precisely and swiftly estimate uncertainties and error states, while a predefined-time anti-saturation compensator is implemented to alleviate actuator saturation. Furthermore, closed-loop stability is guaranteed through rigorous Lyapunov synthesis. Extensive numerical simulations confirm the algorithm’s superiority in terms of control effectiveness.

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Publication Details

Journal
The Aeronautical Journal
Published
2025-11-14
DOI
https://doi.org/10.1017/aer.2025.10091
Primary Topic
Adaptive Control of Nonlinear Systems
Type
article
Field-Weighted Citation Impact
0.00
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article

The design of predefined-time anti-saturation attitude control with disturbance observer for hypersonic morphing vehicles

Horchhong Cheng, Wei Wang, Li Cui, Qingdian Zhang
The Aeronautical Journal
Adaptive Control of Nonlinear Systems
article

The design of predefined-time anti-saturation attitude control with disturbance observer for hypersonic morphing vehicles

Horchhong Cheng, Wei Wang, Li Cui, Qingdian Zhang
article en

Abstract

Abstract This paper addresses the attitude control challenge of hypersonic morphing vehicles (HMVs) with uncertainties and actuator saturation. The primary contribution of this work lies in achieving a predefined settling time while ensuring robust control performance under morphing effects, actuator saturation and disturbances. Firstly, a control-oriented model is established based on the dynamics of HMVs. Subsequently, a nonsingular multivariable sliding mode manifold, utilising a switching function, is designed to attain predefined-time convergence and prevent singularity issues. A disturbance observer with an adaptive law is developed to precisely and swiftly estimate uncertainties and error states, while a predefined-time anti-saturation compensator is implemented to alleviate actuator saturation. Furthermore, closed-loop stability is guaranteed through rigorous Lyapunov synthesis. Extensive numerical simulations confirm the algorithm’s superiority in terms of control effectiveness.

The Aeronautical JournalVol. 130(1344)
Beihang University (CN)
Openalex Percentile: Top 57%
Adaptive Control of Nonlinear Systems
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The design of predefined-time anti-saturation attitude control with disturbance observer for hypersonic morphing vehicles — Horchhong Cheng, Wei Wang, et al. · The Aeronautical Journal (2025) | TGRS Research Map | TGRS