The Study Of Flight Control System For Micro Aerial Vehicle

This paper mainly discusses the control law and system structure of MAV. As experiment, a PCS is designed for a certain MAV.At first this paper introduce the research situation of MAV in the world and then particularly discuss the fixed-wing MAV .At last it stresses to introduce how the software and hardware of control system is designed toward NUAA MAV. This system is based on MCU .digital compass, velocity gyro and GPS.