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Sampurna, Edwin Ramadhani and Pitowarno, Endra and Arini, Nu Rhahida (2011) DESAIN DAN SISTEM PENGENDALIAN PELUNCUR ROKET CERDAS BERDASARKAN KECEPATAN DAN ARAH ANGIN. EEPIS Final Project.

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    At this final task will be analyzed and implementated position control using PID (Proportional, Integratif and Derivative) controller in a plant of two degree-of-freedom Rocket Launcer with joint-Launcer configuration controlled by two DC motor. Movement input of rocket launcer will be controlled by a Mikrocontroler using C program and Matlab Simulink application. The input has given by the form of target position and PID constanta. Controling the rocket launcer use the DC motor which calculated movement direction and regardless dynamic motor constanta. This implementation process border with special purpose of rocket launcher two degrees freedom is designed to be able to perform the specific function rise-down movement and rotates up to 360 degrees. Rocket launcher equipped with sensor enviromment wind velocity and direction to make rocket launchers that could see the wind direction changes so that know where the rocket launching at the right time. Sensor enviromment wind velocity and direction will be used as input to the system for the value of PID control parameters. Data collected from wind speed and direction sensors enviromment as an input is obtained that changes in a degree equal to 2,44. the results are expected to value the PID control parameters that can be used to design a rocket launcher system with a more complex system with feedback purposes.

    Item Type: Article
    Subjects: Q Science > QA Mathematics > QA75 Electronic computers. Computer science
    Q Science > QA Mathematics > QA76 Computer software
    Divisions: Faculty of Engineering, Science and Mathematics > School of Electronics and Computer Science
    Depositing User: Mrs fariny masna
    Date Deposited: 15 Apr 2011 21:09
    Last Modified: 15 Apr 2011 21:09

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