An Introduction to Flight Control of Three-duct Compound UAV

Hu Yanpeng: Since work, I have been engaged in the research of the unmanned aerial vehicle system design, dynamic modeling and flight control. I have successively participated in the research and development of solar powered unmanned aerial vehicle, micro-unmanned helicopter, and compound unmanned aerial vehicle. The main research contents include the overall optimization design, design of flight control and management system, dynamic modeling, flight control law design and simulation, and flight test. I have the rich engineering experience.

内容简介

This book takes a three-rotor compound UAV with tilt-rotor tail as the research object, and studies the dynamic modeling and flight control through the combination of theoretical analysis and flight test. The main contents are as follows: （1） Research on flight dynamics modeling methods, including theoretical modeling methods and system identification modeling methods. In the system identification modeling, the AF25B micro-helicopter is used as the test platform to carry out the relevant frequency sweep tests. Combined with the flight test data, the system identification method is used to identify part of the dynamic model and modify the model. （2） Research on flight control methods, including the control strategy of converting helicopter flight mode to fixed-wing flight mode, the helicopter attitude control method of combining h-infinity loop shaping and dynamic inversion, and the adaptive fuzzy PID position and speed tracking control method based on improved genetic algorithm. （3） The flight path tracking control algorithm and attitude stability control algorithm suitable for fixed-wing flight are further designed.