Perancangan Sistem Kendali Otomatis untuk UAV MiniBe

Authors

  • Aqil Nedhio Wibowo FTMD, ITB
  • Toto Indriyanto FTMD, ITB

Abstract

MiniBe adalah salah satu program dalam riset penguatan inovasi ITB. MiniBe adalah UAV (Unmanned Aerial Vehicle) kecil yang dirancang untuk keperluan surveillance di daerah terpencil dan perbatasan. UAV MiniBe ini merupakan UAV yang unik karena hanya memiliki elevon (gabungan elevator dan aileron) sebagai bidang kendalinya. Dalam jurnal ini, akan dianalisis kestabilan gerak UAV MiniBe pada matra longitudinal dan lateral-direksional dengan model gerak hasil linierisasi. Setelah analisis kestabilan, dirancang sistem kendali otomatis untuk UAV tersebut. Sistem kendali tersebut meliputi Pitch Attitude Hold, Altitude Hold, Airspeed Hold, Yaw Damper dan Turn Coordinator. Sistem kendali otomatis yang dirancang dinyatakan berhasil jika memenuhi kriteria perancangan standar MIL-STD-1979A. Dari berbagai simulasi yang dilakukan dapat diketahui bahwa seluruh sistem kendali otomatis yang dirancang telah memenuhi kriteria perancangan dan memberikan hasil yang memuaskan.

References

Wibowo, Aqil N., Analisis Kestabilan dan Simulasi Gerak UAV Fixed Wing, Laporan Tugas Akhir Program Studi Teknik Dirgantara Institut Teknologi Bandung, 2019.

Pallet, E.H.J., Automatic Flight Control, Blackwell Science Ltd, Oxford, 1993.

Pamadi, Bandu., Performance, Stability, Dynamics and Control of Airplanes. American Institute of Aeronautics and Astronautics., Virginia, 2004.

Blakelock, John H., Automatic Control of Aircraft and Missiles, John Wiley & Sons, Inc., New York, 1965.

William, J.E., The USAF Stability & Control Digital DATCOM - Volume I, User Manual, Airforce Flight Dynamics Laboratory Wright-Patterson Airforce Base, Ohio, 1979.

Department of Defense Interface Standard. 1995. MIL-STD-1797A.

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Published

2019-10-24

Issue

Vol. 2 No. 1 (2019)

Section

Articles

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