Flight Dynamic Modelling and Control System Design for a Flapping Wing Micro Aerial Vehicle at Hover

Author(s):  
Kum Hoe Loh ◽  
Mike Cook
2012 ◽  
Vol 224 ◽  
pp. 510-513
Author(s):  
Wei Zhang ◽  
Ning Jun Fan

This paper deals with the dynamic modeling of a ducted fan vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) and focuses on the dynamic characteristics analyzing in forward flight. A 6-DOF nonlinear model has been established in terms of the forces and moments and the model can be used in the structure and control system design.


2013 ◽  
Vol 483 ◽  
pp. 652-655
Author(s):  
Yi Zhou ◽  
Zhong Xi Hou ◽  
Shang Qiu Shan ◽  
Bo Wang

This paper carried out the control system design of a DFV based on dynamical characteristic analysis, and flight experiments were carried out to validate the performance of the control system. Firstly, the characteristics such as outstanding and control difficulty were pointed out, and then the control strategy such as three forms of translation is proposed. In the end, the controller was realized and tested by a series of experiments, and the excellent performance was demonstrated by the experimental results.


Author(s):  
Margaret A. Abernethy ◽  
Jan Bouwens ◽  
Laurence van Lent

Sign in / Sign up

Export Citation Format

Share Document