Thavai, RahulShaikh, Altamash(12ME48)Syed, Adnan (12ME62)Padwekar, Aamir(13ME133)2016-08-272016-08-272016-04-09http://www.aiktcdspace.org:8080/jspui/handle/123456789/1780ICMTEST-16 International Conference on Modern Trends In Engineering, Science And Technology.Our project consists of plotting various outputs of kinematic and dynamic motion with respect to time . This output is obtained by making a quadcopter to trace a pescribed trajectory in the MATLAB ra13 simulation platform.the centre of the mass of the quadcopter is maintained at the centre of the quadcopter and the following governing kinematic and dynamic equations are pepared. These equations derived are used for the inception of the kinematic and dynamic modelling of the quadcopter made to trace the trajectory. The outputs of the kinematic and dynamic modelling are made the input for the correction of error input and tuning of the PID control system. This closed function PID control system is used for the stabalization of the quadcopter while following a given trajectory and optimize the output of the kinematic and dynamic modelling process for tuning purpose of the control. Index Terms - List key index terms here. No mare than 5.en-USStaff Publication - SoETStaff Publication - MEStudent Publication - SoETStudent Publication - MEArticle