Mode-Recovered Bumpless Transfer Control for Aero-Engines with Switched Models

Z Wu, Y Shi, Z Fei, X Liu - IEEE Transactions on Aerospace and …, 2024 - ieeexplore.ieee.org
According to the multimode characteristics, aeroengines are usually modeled as switched
systems to better reflect the working dynamics, and switched controllers are designed to …

Event-trigger-based adaptive barrier function higher-order global sliding mode control technique for quadrotor UAVs

B Liu, Y Wang, MA Sepestanaki… - … on Aerospace and …, 2024 - ieeexplore.ieee.org
This paper proposes an event-triggered control technique based on an adaptive barrier
function higher-order global sliding mode control for a class of quadrotor unmanned aerial …

Anti-disturbance Event-Triggered Control for Aero-engine Systems via Switched Affine Models

Y Zhao, X Ni, S Wen, B Niu - IEEE Transactions on Aerospace …, 2024 - ieeexplore.ieee.org
This study is focused on the issue of anti-disturbance event-triggered (ADET) control for aero-
engine control systems (AECS) under multiple disturbances. Firstly, a switched affine model …

Gains-Scheduling Tracking Control for Quadrotors Under Ground Effects Via NTSMC-sLPV

L Zhang, T Gao, Z Lin, Y Liang… - IEEE Transactions on …, 2024 - ieeexplore.ieee.org
This paper is devoted to the tracking control problem of a quadrotor in near-ground tasks,
where the aerodynamic force of propellers impaired by ground effects is considered. TAES …

High-Speed Trajectory Tracking Control for Quadrotors via Deep Reinforcement Learning

H Hua, H Zhong, H Zhang, Y Fang… - 2024 39th Youth …, 2024 - ieeexplore.ieee.org
This paper presents a learning-based high-speed trajectory tracking control strategy for
quadrotors, which achieves efficient learning and strong reliability by the collaboration of …

Attitude Tracking of Near-ground Quadrotor: A Switched Linear Parameter Varying Approach

Y Liang, Z Lin, T Gao, Y Dong, Y Ding… - 2024 36th Chinese …, 2024 - ieeexplore.ieee.org
This paper is devoted to the attitude tracking problem of a near-ground quadrotor, where the
aerodynamic force of propellers is impaired under the ground effect. An altitude-dependent …

Observer Design for Two-Dimensional Switched Discrete-Time Linear Systems with Multiple Equilibrium Points

K Liang, J Zhang, L Zhu - 2024 IEEE 13th Data Driven Control …, 2024 - ieeexplore.ieee.org
This paper investigates the observer design problem for two-dimensional switched discrete-
time linear systems with multiple equilibrium points. Firstly, a distributed state observer is …

Smooth Switched Flight Control Design of Fixed-wing Aircraft for Heavy Payload Airdrop

Y Liang, Y Dong, Y Han, T Gao, Y Ma… - 2024 36th Chinese …, 2024 - ieeexplore.ieee.org
This paper investigates the issue of flight control of fixed-wing aircraft (FwA) in heavy
payload airdrop tasks, where smooth control commands are considered for actuators. The …