Analisis Sistem Kendali Terbang dengan Gain Scheduling Pada Pesawat Efek Permukaan

Sayuti Syamsuar


This paper provides an overview of the design of adaptive flight control system of wing in surface effect craft Lippisch configuration 8 passengers capacity during cruise in the low speed and low altitude. The control system will be used the control surface, such as elevator deflection as input and pitch angle deflection as output response or by using engine throttle setting as input and others output response in the longitudinal mode. This paper describes some methodologies control system method and analysis such as PID controller system with gain scheduling approach, and root locus method. The observable matrices (4 x 4) on the longitudinal mode that used in the control system became from aerodynamic derivative parameters of 8 seaters configuration that calculated by DATCOM numerical simulation or wind tunnel test result and dummy data.

Kajian ini merupakan rancangan sistem kendali terbang adaptif pada pesawat efek permukaan konfigurasi Lippisch kapasitas 8 orang saat terbang mendatar pada kecepatan dan ketinggian terbang rendah. Sistem kendali terbang yang digunakan, seperti defleksi elevator sebagai input dan defleksi sudut pitch sebagai respon output atau penggunaan defleksi throttle mesin sebagai input dan parameter respon output lain pada gerak matra longitudinal. Kajian menjelaskan penggunaan beberapa metodologi dan analisis sistem kendali terbang adaptif, seperti kontroler PID dengan pendekatan gain scheduling, dan metoda root locus. Matriks ruang keadaan berukuran (4 x 4) pada matra longitudinal yang digunakan pada sistem kendali terbang adaptif diperoleh dari parameter turunan aerodinamika hasil perhitungan numerik DATCOM atau hasil uji terowongan angin dan data dummy.


kontrol adaptif; efek permukaan; konfigurasi Lippisch; kontroler PID; root locus; neural networks; dan uji terowongan angin

Full Text:



Collu, M., M. H. Patel, and  F. Trarieux. (2007), A Unified Mathematical Model for High Speed Hybrid (Air and Water borne) Vehicles, Cranfield University, United Kingdom

Hassan, M. Y. (2012) Adaptive Control for the 4 th. Class of Control Engineering in the Control and Systems Engineering, Department at the University of Technology CCE CN445

Muhammad, H. (2003), Perancangan Sistem Kendali Otomatik Longitudinal Kapal Bersayap Wing In Surface Effect, Studi Kasus Kapal bersayap: NWIG10B-Wing 01, Departemen Teknik {enerbangan, Fakultas Teknologi Industri, Institut Teknologi Bandung

Muhammad, H. (2005), Technical Report, Design Configuration, Preliminary Design, Part I-A WiSE Aerodynamic Prediction based on DATCOM, LPPM ITB, Bandung

Ogata, K. (1994), Solving Control Engineering Problems with Matlab, Prentice Hall, New Jersey

Priandana, K. and B. Kusumoputro. (2015), Development of Self Organizing Maps Neural Networks Based Control System for a Boat Model, Computational Intelligence and Intelligent Systems Research Group, Department of Electrical Engineering, Faculty of Engineering, Universitas Indonesia, West Java, Journal of Telecommunication, Electronic and Computer Engineering, e-ISSN 2289-8131, Vol. 9 No. 1-3

 Ruijgrok, G. J. J. (1994), Elements of Airplane Performance, Faculty of Aerospace Engineering, Delft University of Technology, Delft University Press.

Sarhan, A., and M. Ashry. (2013), Self-Tuned PID Controller for the Aerosonde UAV Autopilot, International Journal of Engineering Research & Technology (IJERT), Vol. 2 Issue 12, December – 2013, ISSN: 2278-0181

Shin, Y and A. J. Calise. (2005), Application of Adaptive Autopilot Designs for an Unmanned Aerial Vehicle, American Institute of Aeronautics and Astronautics, Georgia

Stewart, L., and D. G. Koenig. (1966), Flight Measured Ground Effect on a Low Aspect Ratio OGEE Wing Including a Comparison with Wind Tunnel Results, NASA Technical Note D-3431, Ames Research Center, Moffet Field, California

Taylor, G. (2003), Re-defining Sea Level: The Hoverwing Wing In Ground Effect Vehicle, Fischer Flugmechanik/AFD Airfoil Development GmbH, Germany, Paper for the Hovercraft Society, Air Cushion Technology Conference & Exhibition, England

Wijiatmoko, G. (2006), Laporan Pengujian WISE-8 di ILST (Eksperimen 123), Laboratorium Aero-Gas Dinamika dan Getaran, BBTA3-BPPT, Serpong 



  • There are currently no refbacks.

Creative Commons License
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.


      Infobase Index  Logo IPI  Home  

Copyright of Warta Ardhia (e-ISSN:2528-4045, p-ISSN:0215-9066) Sekretariat Jurnal Transportasi Udara, Jl. Medan Merdeka Timur No. 5 A Jakarta Pusat 10110. Tlp. (021) 34832944, Fax. (021) 34832968.;

    Creative Commons License 
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.

  Analytics View My Stats