PERANCANGAN AUTOPILOT LATERAL-DIREKSIONAL PESAWAT NIRAWAK LSU-05 (THE DESIGN OF THE LATERAL-DIRECTIONAL AUTOPILOT FOR THE LSU-05 UNMANNED AERIAL VEHICLE)
DOI:
https://doi.org/10.30536/j.jtd.2017.v0.a2760Keywords:
lateral-direksional, autopilot, PIDAbstract
Autopilot pada pesawat dikembangkan berdasarkan pada modus gerak pesawat yaitu modus gerak longitudinal dan lateral-directional. Pada makalah ini, dirancang autopilot pada modus gerak lateral-directional untuk pesawat LSU-05. Autopilot dirancang pada range kecepatan operasi pesawat yaitu 15 m/dtk, 20 m/dtk, 25 m/dtk, dan 30 m/dtk dengan ketinggian 1000 m. Autopilot yang dirancang adalah Roll Attitude Hold, Heading Hold dan Waypoint Following. Autopilot dirancang berdasarkan model linier dalam bentuk state-space. Pengendali yang digunakan adalah pengendali Proportional-Integral-Derivative (PID). Hasil simulasi menunjukan nilai overshoot/undershoot tidak melebihi 5% dan settling time kurang dari 30 detik jika diberikan perintah step.
References
Allerton, D., 2009. Principles of Flight Simulation, John Wiley & Sons Ltd, West Sussex. ISBN: 978-0-470-75436-8.
Duhri, R. A. dan Sasongko, R. A., 2016. Development of Generic Flight Dynamic Mathematical Model for Aircraft Flight Simulation and Analysis. Advance in Aerospace Science and Technology in Indonesia, Vol. I, 144-158.
Eko Budi Purwanto, dkk, 2013, Pemodelan dan Simulasi Sistem Kendali Proportional Integral Derivative untuk Kestabilan Dinamika Terbang, Majalah Sains dan Teknologi Dirgantara Vol. 8 No. 2, 48-59.
Etkin, B. dan Reid, L. D., 1996. Dynamics of Flight Stability and Control, John Wiley & Sons Inc. ISBN: 0-471-03418-5.
Gouthami, E., dan Rani, M.A., 2016. Modeling of an Adaptive Controller for an Aircraft Roll Control System using PID, Fuzzy-PID and Genetic Algorithm. IOSR Journal of Electronics and Communication Engineering (IOSR-JECE) Volume 11, Issue 1, Ver.II, 15-24.
Kada, B. dan Ghazzawi, Y., 2011. Robust PID Controller Design for an UAV Flight Control System, Proceedings of the World Congress on Engineering and Computer Science Vol II, WCECS, October 19-21, San Francisco, USA. ISBN: 978-988-19251-7-6.
Mark Drela, AVL. URL http://web.mit.edu/ drela/Public/web/avl/. Diakses: 14 Pebruary 2017.
Nair, M.P. dan Harikumar, R., 2015. Longitudinal Dynamics Control of UAV, International Conference on Control, Communication & Computing India (ICCC), 19-21 November.
Nelson, R. C., 1998. Flight Stability and Automatic Control, McGraw-Hill, New York. ISBN: 0-07-046218-6.
Ogata, K., 2010. Modern Control Engineering, Prentice Hall, New Jersey. ISBN: 0-13-615673-8.
Pustekbang, LSU-05, LAPAN. URL http:// pustekbang.lapan.go.id. Diakes: 20 Januari 2017.
Sufendi, dkk, 2013. Design and Implementation of Hardware-In-The-Loop-Simulation for UAV Using PID Control Method, International Conference on Instrumentation, Communications, Information Technology, and Biomedical Engineering (ICICI-BME), November 7-8, Bandung.
Tim LSU-05, 2014. Progress Report LAPAN Surveillance UAV (LSU) 05, Pusat Teknologi Penerbangan LAPAN, Bogor.
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2017 Author (s)
This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.
