This paper introduces a drone attitude control system using proportional integral derivative techniques and recycled carbon fiber structure. The carbon fiber usage in the fuselage and wings become more important due to many mechanical properties such as solidity with light weight effectiveness performance. Hence, the stiffness and mass of the module structure could be increase by the carbon fiber implementation of drone. To obtain good sink rate, the weight required to be minimized and optimized. In the drone design, the optimization of the drone will break in case of its pressed to the restrictions or redirect too much that will not talented to carry out as well. The drone design is a vital problem is deflection limitation when gradually insert power to every launch of well trim out the replica. Additionally, the light weight of carbon fiber allows for smooth and easy takeoff and landing with high and sharp maneuver in the behavior of the drone during fighting or any other usage of drone such as during the capture of personal photos reactions. The proposed design contains many components for sensors, interface, radios and arduino controllers. The iteration signals control input calculation and estimation of system states are done on the chip to allow the user for command actions. The results show an effective controlling of drone flight attitude estimation and modifying with noise effects and wind performance during the drone flying.