Automatic landing controller design and simulation of flying-wing unmanned aerial vehicle

Abstract

A method of guidance and control for automatic landing of flying-wing unmanned aerial vehicle (UAV) is proposed in this paper. Based on wind tunnel data of a flying-wing aircraft, small disturbance equations of the flying-wing aircraft is built using MATLAB. With the help of the model, automatic landing plan and control law is designed. Simulation and analysis are finished based on non-linear equations. The final simulation results show that the guidance and control law can meet the requirements of automatic landing of UAV, and has excellent static and dynamic performances.

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Cite this paper

@article{Jianfeng2013AutomaticLC, title={Automatic landing controller design and simulation of flying-wing unmanned aerial vehicle}, author={Zhang Jianfeng and Jia Caijuan}, journal={Proceedings of 2013 2nd International Conference on Measurement, Information and Control}, year={2013}, volume={02}, pages={893-896} }