Pengendalian 3-Axis Reaction Wheel Satelit LAPAN-TUBSAT A1 Menggunakan Kendali PID Teroptimasi Algoritma Genetika

Article Sidebar

PDF
Published: Apr 9, 2019
DOI: https://doi.org/10.47313/jig.v21i1.581
Keywords:
Algoritma genetika ADCS LAPAN-TUBSAT A1

Main Article Content

Yulio Ramadhan
Program Studi Teknik Fisika, Universitas Nasional
Hari Hadi Santoso
Program Studi Teknik Fisika, Universitas Nasional
Erna Kusuma Wati
Program Studi Teknik Fisika, Universitas Nasional

Abstract

Reaction wheel merupakan aktuator aktif yang digunakan pada subsistem Attitude Determination and Control System (ADCS) Satelit, pada penelitian ini pengendalian reaction wheel disimulasikan dengan menggunakan kendali PID dan penalaan menggunakan Algoritma Genetika dengan populasi awal sebanyak 100 populan, laju crossover 0.8, konstanta mutasi 0.01, kriteria penghenti adalah 50 generasi dengan fitness function berdasarkan indeks performansi PID yaitu ITAE. Pengendalian Reaction Wheel pada lingkar tertutupnya dengan kendali PID yang teroptimasi Algoritma Genetika memiliki karakteristik respon transien yaitu rise time 11 detik, setlling time 91 detik, overshoot 33.2% dengan indeks performansi ITAE sebesar 481.9479. Dengan menggunakan simulator Smart Nanosatellite Attitude Propagator (SNAP) berbasis MATLAB, dilakukan simulasi dinamis menggunakan model 3-axis reaction wheel sebagai aktuatornya. Satelit LAPAN –TUBSAT A1 digunakan sebagai objek pengendalian, dilakukan simulasi dengan menskenariokan bahwa satelit dalam keadaan tumble memiliki inisial kecepatan sudut [0.5 0.5 0.5] °/detik kemudian dilakukan detumbling yaitu membuat kecepatan sudut satelit menjadi [0 0 0]°/detik. Sumbu roll dan yaw memiliki error yang cukup besar yaitu direntang 1 rad/s dan -1 rad/s sedangkan sumbu pitch memiliki error kecil direntang 1.5x10−3 rad/s dan −1.5x10−3 rad/s.

Article Details

How to Cite
Ramadhan, Y., Santoso, H. H., & Wati, E. K. (2019). Pengendalian 3-Axis Reaction Wheel Satelit LAPAN-TUBSAT A1 Menggunakan Kendali PID Teroptimasi Algoritma Genetika. Jurnal Ilmiah Giga, 21(1), 24–32. https://doi.org/10.47313/jig.v21i1.581
Issue
Vol. 21 No. 1 (2018): Volume 21 Edisi 1 Tahun 2018
Section
Articles

Authors who publish with this journal agree to the following terms:

  1. Authors retain copyright and grant the journal right of first publication with the work simultaneously licensed under a Creative Commons Attribution License that allows others to share the work with an acknowledgment of the work's authorship and initial publication in this journal.
  2. Authors are able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the journal's published version of the work (e.g., post it to an institutional repository or publish it in a book), with an acknowledgment of its initial publication in this journal.
  3. Authors are permitted and encouraged to post their work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of published work (See The Effect of Open Access).

References

"What Is a Satellite?," National Aeronautics and Space Administration, 8 February 2018. [Online]. Available: https://www.nasa.gov/audience/forstudents/k-4/stories/nasa-knows/what-is-a-satellite-k4.html. [Accessed 5 March 2018].

S. R. Starin, Attitude Determination and Control Systems, Microcosm, 2010.

N. Imroatul and H. Nurhadi, "Komparasi Sistem Kontrol Satelit (ADCS) dengan Metode Kontrol PID dan Sliding-PID," Jurnal Teknik POMITS, vol. I, no. 1, 2012.

S. Li, J. Yuan, J. Luo and W. Ma, "Satellite Attitude Control through Evolving a

Neural Network," in International Conference on Mechatronics and Automation,

Xi'an, 2010.

"Types of Orbits," European Space Agency, 17 April 2017. [Online]. Available:

https://www.esa.int/Our_Activities/Space_Transportation/Types_of_orbits.

Accessed 6 March 2018].

H. Riebeek, "Catalog of Earth Satellite Orbits," Earth Observatory, National

Aeronautics and Space Administration, 4 September 2009. [Online]. Available:

https://earthobservatory.nasa.gov/Features/OrbitsCatalog/. [Accessed 6 March

.

R. Mohsenipour, H. Nemati and dkk, "Attitude Control of a Flexible Satellite by

Using Robust Control Design Methods," Intelligent Control and Automation, vol. 4, no. 3, 2013.

R. E. Kalman, A New Approach to Linear Filtering and Prediction Problems,

Baltimore: Research Institute for Advance Study, 1960.

K. J. Astrom and T. Hugglund, PID Controllers: Theory, Design, and Tuning,

Instrument Society of America, 1995.

S. Kusumadewi, Artificial Intelligence (Teknik dan Aplikasinya), Yogyakarta:

Graha Ilmu, 2003. Te-Chin Jan, “(12) United States Patent,” US 6285630 B1, 2002.

E. Stella Ogochukwu, A. Desmond Okechukwu, and O. Godfrey Nnaegbo,

“Construction And Testing Of Ultrasonic Bird Repeller,” J. Nat. Sci. Res.

www.Online), vol. 2, no. 9, pp. 2225–921, 2012.

I. Buyung and A. W. Soejono, “Area Persawahan Dengan Menggunakan

Gelombang Ultrasonik Berbasis Mikrokontroler Atmega168,” pp. 121–134, 2012.

A. E. Waluyo et al., “Rancang Bangun Prototype Panel Surya Sebagai Alat,” pp. 1–4, 2010.

S. Trajectory, P. Dan, F. Pada, and R. Obstacle, “Journal of Control and Network Systems,” vol. 4, no. 1, pp. 31–38, 2015.

Y. A. Zulfiadi, “Prototype Alat Pengusir Hama Burung Berbasis Mikrokontroler

Atmega8,” 2012.

C. F. Nome and F.- Sensore, “FC-04 Sensore Schede sensori,”2–5, 2014.

Tatsuro Baba, “Time-Frequency Analysis Using Short Time Fourier Transform,”

Open Acoust. J., vol. 5, pp. 32–38, 2012.

A. G. De Oliveira et al., “Bird acoustic activity detection based on morphological

filtering of the spectrogram,” Appl. Acoust., vol. 98, pp. 34–42, 2015.