Optimization pitch angle controller of rocket system using improved differential evolution algorithm
Pitch angle of rocket system is the important parts of the rocket. This part corresponds to the movement of the rocket system. Rocket system is fell into multi-input and multi-output (MIMO) system. The most challenge factor in MIMO system is designing the controller, if the design is not appropriate...
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| Main Authors: | , , |
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| Format: | EJournal Article |
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Universitas Ahmad Dahlan,
2017-03-31.
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| LEADER | 02075 am a22002893u 4500 | ||
|---|---|---|---|
| 001 | IJAIN_83_ijain_v3i1_p27-34 | ||
| 042 | |a dc | ||
| 100 | 1 | 0 | |a Lastomo, Dwi |e author |
| 100 | 1 | 0 | |e contributor |
| 700 | 1 | 0 | |a Setiadi, Herlambang |e author |
| 700 | 1 | 0 | |a Djalal, Muhammad Ruswandi |e author |
| 245 | 0 | 0 | |a Optimization pitch angle controller of rocket system using improved differential evolution algorithm |
| 260 | |b Universitas Ahmad Dahlan, |c 2017-03-31. | ||
| 500 | |a https://ijain.org/index.php/IJAIN/article/view/83 | ||
| 520 | |a Pitch angle of rocket system is the important parts of the rocket. This part corresponds to the movement of the rocket system. Rocket system is fell into multi-input and multi-output (MIMO) system. The most challenge factor in MIMO system is designing the controller, if the design is not appropriate, it may lead to the unstable condition. Hence, appropriate and robust control design is inevitable. This paper introduces PID controller as pitch angle control of rocket system. Furthermore, PID controller parameter is optimized using improved differential evolution algorithm (IDEA). To analyze the performance of rocket system, time domain simulation is implemented. From the simulation result, it is found by using PID controller based on IDEA, the performance of pitch angle of rocket system is enhanced. | ||
| 540 | |a Copyright (c) 2017 Dwi Lastomo, Herlambang Setiadi, Muhammad Ruswandi Djalal | ||
| 540 | |a https://creativecommons.org/licenses/by-sa/4.0 | ||
| 546 | |a eng | ||
| 690 | |a Improved differential evolution algorithm, Pitch angle, Rocket system, PID controller | ||
| 655 | 7 | |a info:eu-repo/semantics/article |2 local | |
| 655 | 7 | |a info:eu-repo/semantics/publishedVersion |2 local | |
| 655 | 7 | |2 local | |
| 786 | 0 | |n International Journal of Advances in Intelligent Informatics; Vol 3, No 1 (2017): March 2017; 27-34 | |
| 786 | 0 | |n 2548-3161 | |
| 786 | 0 | |n 2442-6571 | |
| 787 | 0 | |n https://ijain.org/index.php/IJAIN/article/view/83/ijain_v3i1_p27-34 | |
| 856 | 4 | 1 | |u https://ijain.org/index.php/IJAIN/article/view/83/ijain_v3i1_p27-34 |z Get Fulltext |