Adaptive Trajectory Tracking Control for Unmanned Airships With Input Saturation and Quantization

ABSTRACT This article proposes a novel adaptive robust nonlinear trajectory‐tracking control strategy for an unmanned airship subject to actuator saturation, input quantization, unknown time‐varying disturbances, and model uncertainties. An auxiliary system is first developed to solve the actuator saturation. Then, an adaptive nonsingular terminal sliding mode controller is designed based on the barrier function. The utilized adaptive law eliminates the need to assume disturbance upper bounds, avoids overestimating control gains, reduces chattering, and allows for a stable zero neighborhood of predefined sliding variables. Due to limitations in communication bandwidth, a quantizer is used to quantize the control commands. The key feature of this method is its strong capability for saturation compensation and precise trajectory tracking. Finite‐time stability is theoretically proven using the Lyapunov method, and the superiority of the control algorithm is demonstrated through numerical simulations.

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Institutions

Publication Details

Journal
International Journal of Robust and Nonlinear Control
Published
2025-04-16
DOI
https://doi.org/10.1002/rnc.7988
Citations
2
Primary Topic
Aerospace Engineering and Energy Systems
Type
article
Field-Weighted Citation Impact
9.99

Funders

Controls
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article

Adaptive Trajectory Tracking Control for Unmanned Airships With Input Saturation and Quantization

Hongyan Li, Chang Zhang, Jiang Wang
2 citations
International Journal of Robust and Nonlinear Control
Aerospace Engineering and Energy Systems
9.99
article

Adaptive Trajectory Tracking Control for Unmanned Airships With Input Saturation and Quantization

Hongyan Li, Chang Zhang, Jiang Wang
article en
2 citations

Abstract

ABSTRACT This article proposes a novel adaptive robust nonlinear trajectory‐tracking control strategy for an unmanned airship subject to actuator saturation, input quantization, unknown time‐varying disturbances, and model uncertainties. An auxiliary system is first developed to solve the actuator saturation. Then, an adaptive nonsingular terminal sliding mode controller is designed based on the barrier function. The utilized adaptive law eliminates the need to assume disturbance upper bounds, avoids overestimating control gains, reduces chattering, and allows for a stable zero neighborhood of predefined sliding variables. Due to limitations in communication bandwidth, a quantizer is used to quantize the control commands. The key feature of this method is its strong capability for saturation compensation and precise trajectory tracking. Finite‐time stability is theoretically proven using the Lyapunov method, and the superiority of the control algorithm is demonstrated through numerical simulations.

International Journal of Robust and Nonlinear ControlVol. 35(13)
Beijing Institute of Technology (CN)
National Natural Science Foundation of China
Openalex Percentile: Top 3%
Aerospace Engineering and Energy Systems
9.99
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