Nonlinear Generalized Predictive Control for a Novel Thrust-vectoring Hexarotor Using Super-twisting ESO

Thrust-vectoring multirotor is the current cuttingedge focus of research in the field of multirotor. This technology promises advancements such as over-actuated dynamics, decoupling of position and attitude control, and the ability to track 6-Dof trajectories. Building upon our previous work on thrust-vectoring quadrotor, this paper introduces a novel thrust-vectoring hexarotor configuration. We propose a nonlinear generalized predictive control method utilizing the super-twisting extended state observer (STESO). The stability of our closed-loop system is rigorously established through theoretical analysis. To validate the practical applicability of our approach, simulation for 6-Dof trajectory tracking of the thrust-vectoring hexarotor is conducted using sophisticated high-fidelity dynamics simulation software. This simulation serve to affirm the effectiveness of our proposed system in achieving precise trajectory control and maneuverability in various flight scenarios.

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Publication Details

Published
2024-11-03
DOI
https://doi.org/10.1109/iecon55916.2024.10905896
Primary Topic
Spacecraft Dynamics and Control
Type
article
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article

Nonlinear Generalized Predictive Control for a Novel Thrust-vectoring Hexarotor Using Super-twisting ESO

Zhan Li, Yipeng Yang, Zonglin Li
Spacecraft Dynamics and Control
article

Nonlinear Generalized Predictive Control for a Novel Thrust-vectoring Hexarotor Using Super-twisting ESO

Zhan Li, Yipeng Yang, Zonglin Li
article en

Abstract

Thrust-vectoring multirotor is the current cuttingedge focus of research in the field of multirotor. This technology promises advancements such as over-actuated dynamics, decoupling of position and attitude control, and the ability to track 6-Dof trajectories. Building upon our previous work on thrust-vectoring quadrotor, this paper introduces a novel thrust-vectoring hexarotor configuration. We propose a nonlinear generalized predictive control method utilizing the super-twisting extended state observer (STESO). The stability of our closed-loop system is rigorously established through theoretical analysis. To validate the practical applicability of our approach, simulation for 6-Dof trajectory tracking of the thrust-vectoring hexarotor is conducted using sophisticated high-fidelity dynamics simulation software. This simulation serve to affirm the effectiveness of our proposed system in achieving precise trajectory control and maneuverability in various flight scenarios.

Harbin Institute of Technology (CN)
Affordable and clean energy
Openalex Percentile: Top 53%
Spacecraft Dynamics and Control
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