* Corresponding Author
Hide
Show all
Identifikasi Model dari Pesawat Udara Tanpa Awak Sayap Tetap Jenis Bixler
https://doi.org/10.22146/ijeis.7152 Abdul Majid(1*), Raden Sumiharto(2), Setyawan Bekti Wibisono(3)
(1)
(2) Jurusan Ilmu Komputer dan Elektronika, FMIPA UGM
(3) Diploma III Teknik Mesin, Sekolah Vokasi UGM
(*) Corresponding Author
Abstract
Flight model is one of importing thing in fixed-wing unmanned aerial vehicle (UAV) control system development, mainly in the aircraft autopilot. Through this flight model, the aircraft motion can be represented and simulated.
In this research, the flight model is obtained through system identification and system modelling of Bixler fixed-wing unmanned aerial vehicle. System identification is based on experiment data and use state-space model structure. There are three stages in this research, aircraft motion system modelling, flight data collecting, and flight model identification. Through those three stages, Bixler fixed-wing unmanned aerial vehicle flight model is obtained as represented in two modes, longitudinal mode and lateral mode
The Bixler fixed-wing unmanned aerial vehicle longitudinal mode flight model is obtained using 13 parameters. The lateral mode is obtained using 11 parameters. All modes are in 4th order state space model structure.
Keywords
Full Text:
PDFReferences
Ljung L., 2011, System Identification Toolbox™ User’s Guide, The MathWorks, Inc., Natick.
[2] Söderström T. dan Stoica P. , 2001, System Identification, 2, Prentince Hall International, London.
[3] Masiero C., 2012, Matlab System Identification Toolbox Quickstart, http://automatica.dei.unipd.it/tl_files/utenti2/masieroChiara/Miscellanea/Matlab_SysId_Tutorial.pdf, diakses tanggal 23 November 2013.
[4] McLean, D., 1990, Automatic Flight Control System, Prentice Hall Inc.
[5] Hobbyking, 2011, Bixler v1.1 EPO 1400mm, http://hobbyking.com/hobbyking/store/__16543__Bixler_v1_1_EPO_1400mm_RTF_Mode_1_Throttle_Right_Radio_.html, diakses pada 20 November 2013..
[6] Pratama F., 2013, Sistem Referensi Air Data, Attitude, And Heading Reference System Pada Pesawat Terbang Tanpa Awak, Skripsi, Fakultas Matematika dan Ilmu Pengetahuan Alam, Universitas Gadjah Mada, Yogyakarta.
[7] Sparkfun, 2013, Micro SD Shield, https://www.sparkfun.com/products/9899, diakses tanggal 1 November 2013.
[8] Smith, M. S. dan Moes, T. R., 2003, Real-time Stability and Control Derivative Extraction from F15 Flight Data. AIAA Atmospheric Flight Mechanics Conference, AIAA-2003-5701. [9] Oksa, M., 2012. Identifikasi Sistem Pada Perilaku Pesawat Terbang Tanpa Awak, Skripsi, Fakultas Matematika dan Ilmu Pengetahuan Alam, Universitas Gadjah Mada.
[10] Tischler, M. B., 2006, Aircraft and Rotorcraft System Identification, Engineering Methods with Flight Test Examples, American Institute of Aeronautics and Astronautics.
DOI: https://doi.org/10.22146/ijeis.7152
Article Metrics
Abstract views : 2326
| 
views : 3154
Refbacks
- There are currently no refbacks.
Copyright (c) 2015 IJEIS - Indonesian Journal of Electronics and Instrumentation Systems
This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.
View My Stats1