11   Artículos

 
en línea
Yongyong Zhao, Jinghua Wang, Guohua Cao and Xu Yao    
This study introduces a reduced-order leg dynamic model to simplify the controller design and enhance robustness. The proposed multi-loop control scheme tackles tracking control issues in legged robots, including joint angle and contact-force regulation,... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Zhiyuan Hu, Peng Yu, Guohua Xu, Yongjie Shi, Feng Gu and Aijun Zou    
Tiltrotors permit aircrafts to operate vertically with lift, yet convert to ordinary forward flight with thrust. The challenge is to design a tiltrotor blade yielding maximum lift and thrust that converts smoothly without losing integrity or efficiency. ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yucheng Yang, Guohua Xu, Yongjie Shi and Zhiyuan Hu    
This study develops a hybrid solver with reversed overset assembly technology (ROAT), a viscous vortex particle method (VVPM), and a CFD program based on the URNS method, in order to study the aerodynamic and acoustic characteristics of coaxial rigid rot... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yingkai Xia, Zhemin Huang, Kan Xu, Guohua Xu and Ye Li    
This paper proposes a novel three-dimensional trajectory tracking control methodology for a heterogeneous X-rudder autonomous underwater vehicle (XAUV) that can achieve finite-time convergence, complex actuator dynamics handling, and energy-efficient opt... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Peng Yu, Zhiyuan Hu, Guohua Xu and Yongjie Shi    
Due to the small tilt angle, a tiltrotor operates in non-axial flow conditions during shipboard take-off and landing. The non-uniformity of the blade?s air-load is high, resulting in structural deformation with high fluctuation frequency, affecting the r... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yan Sun, Yongjie Shi and Guohua Xu    
The accurate prediction of helicopter rotor blade?vortex interaction (BVI) noise is challenging. This paper presents an implementation of the seventh-order improved weighted essentially non-oscillatory (WENO-Z) scheme for predicting rotor BVI noise using... ver más
Revista: Aerospace    Formato: Electrónico

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