Results 271 to 280 of about 2,244,717 (304)
Some of the next articles are maybe not open access.
Research on active vibration control of flexible wing based on MFC actuator
International Journal of Applied Electromagnetics and Mechanics, 2020An active vibration control scheme was proposed based on Macro Fiber Composite (MFC) actuators for the bending and torsional vibration control of large flexible lightweight wing structures.
Yajun Luo +5 more
semanticscholar +1 more source
Observer-Based Adaptive Control for a Coupled PDE–ODE System of a Flexible Wing
IEEE Transactions on Systems, Man, and Cybernetics: SystemsThis article proposes an adaptive observer-based control to address the PDE–ODE coupled system of a flexible wing, where external disturbances and references have unknown frequencies, amplitudes, and phases. An exosystem is defined for the above signals,
Tingting Meng +3 more
semanticscholar +1 more source
Mathematics
Fractional-order four-wing (FO 4-wing) systems are of significant importance due to their complex dynamics and wide-ranging applications in secure communications, encryption, and nonlinear circuit design, making their control and stabilization a critical
M. Vu +5 more
semanticscholar +1 more source
Fractional-order four-wing (FO 4-wing) systems are of significant importance due to their complex dynamics and wide-ranging applications in secure communications, encryption, and nonlinear circuit design, making their control and stabilization a critical
M. Vu +5 more
semanticscholar +1 more source
International Journal of Robust and Nonlinear Control, 2019
For achieving the accurate trajectory tracking of the flexible wing unmanned aerial vehicle in the complicated missions, especially the vertical component, a feedforward compensation unit–based active disturbance rejection control (ADRC) is proposed.
Hao Sun +4 more
semanticscholar +1 more source
For achieving the accurate trajectory tracking of the flexible wing unmanned aerial vehicle in the complicated missions, especially the vertical component, a feedforward compensation unit–based active disturbance rejection control (ADRC) is proposed.
Hao Sun +4 more
semanticscholar +1 more source
An Online Reinforcement Learning Wing-Tracking Mechanism for Flexible Wing Aircraft
International Symposium on Robotic and Sensors Environments, 2019Flexible wing aircraft are gaining an increasing interest due to their salient features, such as inexpensive market price, low-cost operation, in-flight robustness, multi-purpose use, and their ability to operate with very little infrastructure.
M. Abouheaf +2 more
semanticscholar +1 more source
Journal of Vibration and Control, 2021
The vibration control problem was investigated in this study in the presence of unknown loss of actuator effectiveness fault and loss of sensor effectiveness fault in a flexible aircraft wing system. A series of partial differential equations was used as
Shiqi Gao, Jinkun Liu
semanticscholar +1 more source
The vibration control problem was investigated in this study in the presence of unknown loss of actuator effectiveness fault and loss of sensor effectiveness fault in a flexible aircraft wing system. A series of partial differential equations was used as
Shiqi Gao, Jinkun Liu
semanticscholar +1 more source
Experimental Aeroelastic Benchmark of a Very Flexible Wing
AIAA Journal, 2022Or Avin +4 more
semanticscholar +1 more source
Large deformation and failure analysis of the corrugated flexible composite skin for morphing wing
Engineering structures, 2023Tian Liu +3 more
semanticscholar +1 more source

