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   Autonomous attitude control of a quadcopter unmanned aerial vehicle (UAV)  
   
نویسنده mustapa z. ,saat s.
منبع journal of telecommunication, electronic and computer engineering - 2015 - دوره : 7 - شماره : 2 - صفحه:153 -160
چکیده    This paper discusses on the development of autonomous attitude control of a quadcopter unmanned aerial vehicle (uav). the quadcopter system is modeled using state-space equations and simulated in matlab/simulink. the paper describes the controller design method for automatic attitude control of uav to enable the system to operate based on the task of the navigation unit. to be specific,the pid controller is designed to control and stabilize quadcopter attitude. then quadcopter acceleration control system will be designed. this system is designed by combining the attitude control on quadcopter rigid body with acceleration control quadcopter movement. through the obtained results,the proposed pid controller managed to control the acceleration of quadcopter well.
کلیدواژه Attitude Control; PID; Quadcopter; UAV system
آدرس faculty of electronic and computer engineering,universiti teknikal malaysia melaka (utem),durian tunggal, Malaysia, faculty of electronic and computer engineering,universiti teknikal malaysia melaka (utem),durian tunggal, Malaysia
 
     
   
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