Adaptive Finite-Time Preassigned Performance Control for Hypersonic Vehicles with Lumped Perturbations

This paper proposes an adaptive finite-time preassigned performance control (PPC) approach to solve the attitude control problem of hypersonic vehicles (HSVs) suffering from lumped disturbances. A specific preassigned performance function guaranteeing finite-time stability and small overshoot is presented to constrain the attitude tracking errors. Moreover, a novel synchronous disturbance estimation is presented to build a disturbance observer (DO). Based on the devised preassigned performance function and the information from the DO, an adaptive finite-time preassigned performance controller is devised to solve the attitude control problem. Finally, numerical examples demonstrate the validity of the presented algorithm.

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Publication Details

Published
2024-12-12
DOI
https://doi.org/10.1109/icarcv63323.2024.10821624
Citations
1
Primary Topic
Advanced Control Systems Optimization
Type
article
Field-Weighted Citation Impact
0.33

Funders

Controls
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article

Adaptive Finite-Time Preassigned Performance Control for Hypersonic Vehicles with Lumped Perturbations

Rugang Tang, Zheng Wang, Xin Ning, Chengfeng Luo
1 citations
Advanced Control Systems Optimization
0.33
article

Adaptive Finite-Time Preassigned Performance Control for Hypersonic Vehicles with Lumped Perturbations

Rugang Tang, Zheng Wang, Xin Ning, Chengfeng Luo
article en
1 citations

Abstract

This paper proposes an adaptive finite-time preassigned performance control (PPC) approach to solve the attitude control problem of hypersonic vehicles (HSVs) suffering from lumped disturbances. A specific preassigned performance function guaranteeing finite-time stability and small overshoot is presented to constrain the attitude tracking errors. Moreover, a novel synchronous disturbance estimation is presented to build a disturbance observer (DO). Based on the devised preassigned performance function and the information from the DO, an adaptive finite-time preassigned performance controller is devised to solve the attitude control problem. Finally, numerical examples demonstrate the validity of the presented algorithm.

Northwestern Polytechnical University (CN), Northwest Institute of Mechanical and Electrical Engineering (CN)
National Natural Science Foundation of China, National Key Laboratory of Science and Technology on Communications
Climate action
Openalex Percentile: Top 37%
Advanced Control Systems Optimization
0.33
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