Predefined-time emotion controller based on vertical takeoff and landing system

In this paper, a predefined-time emotion controller (PTEC) is proposed for the control of vertical takeoff and landing system (VTOL). Firstly, the double closed-loop mathematical model of VTOL is introduced. Sliding mode controller (SMC) with a dynamic boundary layer and predefined-time sliding mode controller (PTSMC) are designed for the voltage-current inner-loop (VCIL) and the current-angle outer-loop (CAOL) of the VTOL, respectively. It is proved that the VTOL with the proposed method can converge within predefined-time. Secondly, a continuous radial basis function emotional neural network (CRBENN) with better accuracy than radial basis function neural network (RBFNN) is adopted to approximate the equivalent control term of PTSMC to ensure the control of VTOL with partial unknown dynamics in the model. The update rate of CRBENN is designed by the Lyapunov method, and the whole system stability is ensured. Finally, both of the simulations and the physical experiments show that the VTOL can achieve the desired angle within a predefined-time and has good performance.

Authors

Institutions

Publication Details

Journal
Proceedings of the Institution of Mechanical Engineers Part I Journal of Systems and Control Engineering
Published
2025-11-14
DOI
https://doi.org/10.1177/09596518251383243
Primary Topic
Adaptive Control of Nonlinear Systems
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Predefined-time emotion controller based on vertical takeoff and landing system

Shijian Gao, Mingxing Gao, Yuan Feng, Chao Jia
Proceedings of the Institution of Mechanical Engineers Part I Journal of Systems and Control Engineering
Adaptive Control of Nonlinear Systems
article

Predefined-time emotion controller based on vertical takeoff and landing system

Shijian Gao, Mingxing Gao, Yuan Feng, Chao Jia
article en

Abstract

In this paper, a predefined-time emotion controller (PTEC) is proposed for the control of vertical takeoff and landing system (VTOL). Firstly, the double closed-loop mathematical model of VTOL is introduced. Sliding mode controller (SMC) with a dynamic boundary layer and predefined-time sliding mode controller (PTSMC) are designed for the voltage-current inner-loop (VCIL) and the current-angle outer-loop (CAOL) of the VTOL, respectively. It is proved that the VTOL with the proposed method can converge within predefined-time. Secondly, a continuous radial basis function emotional neural network (CRBENN) with better accuracy than radial basis function neural network (RBFNN) is adopted to approximate the equivalent control term of PTSMC to ensure the control of VTOL with partial unknown dynamics in the model. The update rate of CRBENN is designed by the Lyapunov method, and the whole system stability is ensured. Finally, both of the simulations and the physical experiments show that the VTOL can achieve the desired angle within a predefined-time and has good performance.

Proceedings of the Institution of Mechanical Engineers Part I Journal of Systems and Control EngineeringVol. 240(2)
Tianjin University of Science and Technology (CN), Tianjin University of Technology and Education (CN), Tianjin University of Technology (CN), Beijing Machine Tool Research Institute (CN)
Openalex Percentile: Top 57%
Adaptive Control of Nonlinear Systems
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.