Altitude controller design for quadcopter UAV

This paper discusses on attitude control of a quadcopter unmanned aerial vehicle (uav) in real time application. newton-euler equation is used to derive the model of system and the model characteristic is analyzed. the paper describes the controller design method for the hovering control of uav automatic vertical take-off system. in order to take-off the quadcopter and stable the altitude,pid controller has been designed. the scope of study is to develop an altitude controller of the vertical take-off as realistic as possible. the quadcopter flight system has nonlinear characteristics. a simulation is conducted to test and analyze the control performance of the quadcopter model. the simulation was conducted by using mat-lab simulink. on the other hand,for the real time application,the pci-1711 data acquisition card is used as an interface for controller design which routes from simulink to hardware. this study showed the controller designs are implemented and tuned to the real system using real time windows target approach by mat-lab simulink. © 2015 penerbit utm press. all rights reserved.