Robust control of gust-induced vibration of highly flexible aircraft

T He, W Su - Aerospace Science and Technology, 2023 - Elsevier
This paper mainly addresses the gust suppression and alleviation of highly flexible aircraft
using the model predictive controller (MPC) based on linear parameter-varying (LPV) …

LPV model-based adaptive MPC of an eVTOL aircraft during tilt transition subject to motor failure

S Qu, G Zhu, W Su, SSM Swei - International Journal of Control …, 2023 - Springer
This paper applies novel LPV (linear parameter-varying) model and MPC (model predictive
control) methods to a tilt-transition process with rotor failure for electric vertical take-off and …

Model-assisted online optimization of gain-scheduled pid control using nsga-ii iterative genetic algorithm

S Qu, T He, G Zhu - Applied Sciences, 2023 - mdpi.com
In the practical control of nonlinear valve systems, PID control, as a model-free method,
continues to play a crucial role thanks to its simple structure and performance-oriented …

Nonlinear modeling and designing transition flight control scenarios for a dual thrust hybrid UAV

N Mohammadi, M Tayefi, M Zhu - International Journal of Intelligent …, 2024 - Springer
Researchers have recently focused on studying the flight dynamics and control of
multicopters and fixed-wing aerial vehicles. However, investigating the transition phase …

Mixed Model Predictive Control and Data-Driven Control of a Tiltrotor eVTOL Aircraft

S Qu, T He, W Su - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
An hybrid control scheme that integrates model-based control and data-driven control is
proposed for electric vertical takeoff and landing (eVTOL) tiltrotor aircraft in this work. The …

Evaluating one engine inoperative conditions in subscale electric vertical take-off and landing aircraft: An in-depth tethered hover test analysis

Y Kang, A Cho, S Choi, Y Kim, J Bae… - Proceedings of the …, 2024 - journals.sagepub.com
The direction of propeller rotation in a distributed electric-powered vertical take-off and
landing (eVTOL) aircraft significantly influences control forces and induced drag during both …

Asynchronous switched LPV control for quad-tilt rotor UAVs against actuator faults and persistent external disturbances

L Nie, H Wang, Z Duan - 2024 36th Chinese Control and …, 2024 - ieeexplore.ieee.org
An asynchronous switched linear parameter-varying (LPV) fault-tolerant control method is
proposed for quad-tilt rotor UAVs to address actuator faults and persistent external …

Polytopic LPV Model-Based Control Design for Hypersonic Vehicle in the Morphing Phase

X Gou, X Zhang, S Lv, L Cui, Q Zhang - Journal of Control Engineering …, 2023 - ceai.srait.ro
In this paper, considering the phenomenon of unsteady attitude control for the hypersonic
morphing vehicle (HMV) with model parameters uncertainties and unknown disturbance in …