Browsing by Author "Padwekar, Aamir(13ME133)"

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    Kinematic and Dynamic Modeling of a Quad copter following a trajectory using MATLAB
    (International Journal on Recent and Innovation Trends in Computing and Communication, 2016-04) Thavai, Rahul; Shaikh, Altamash(12ME48); Syed, Adnan (12ME62); Padwekar, Aamir(13ME133)
    Our task comprises of plotting different yields of kinematic and element movement concerning time. This yield is acquired by making a quad copter to follow an endorsed direction in the MATLAB ra13 reenactment stage. The focal point of the mass of the quad copter is kept up at the focal point of the quad copter and the accompanying administering kinematic and element mathematical statements are readied. These comparisons inferred are utilized for the beginning of the kinematic and element displaying of the quad copter made to follow the direction. The yields of the kinematic and element demonstrating are made the data for the amendment of blunder info and tuning of the PID control framework. This shut capacity PID control framework is utilized for the adjustment of the quad copter while taking after a given direction and advance the yield of the kinematic and element demonstrating process for tuning reason for the control.
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    Kinematic and Dynamic Modeling of a Quadcopter following a trajectory using MATLAB
    (Vishwatmak Om Gurudev College of Engineering, 2016-04-09) Thavai, Rahul; Shaikh, Altamash(12ME48); Syed, Adnan (12ME62); Padwekar, Aamir(13ME133)
    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.
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    Kinematic, dynamic modeling and simulation of quadcopter
    (AIKTC, 2016-05) Thavai, Rahul; Shaikh, Altamash(12ME48); Syed, Adnan (12ME62); Padwekar, Aamir(13ME133)
    Project consists of plotting various outputs of kinematic and dynamic motion with respect to time. This output is obtained by making a quad copter to trace a prescribed trajectory in the MATLAB simulation platform the centre of the mass of the quad copter is maintained at the centre of the quadcopter and the following governing kinematic and dynamic equations are prepared. These equations derived are used for the inception of the kinematic and dynamic modeling of the quad copter made to trace the trajectory. The outputs of the kinematic and dynamic modeling 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 stabilization of the quad copter while following a given trajectory and optimize the output of the kinematic and dynamic modeling process for tuning purpose of the control.