27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-6.3.2

DEVELOPMENT OF A MORPHING FLYING PLATFORM FOR ADAPTIVE CONTROL SYSTEM STUDY

T. Mulyanto, M. L. I. Nurhakim, R. A. Sasongko
Institute of Technology Bandung, Indonesia

Keywords: preliminary design, mini-uav, morphing aircraft, variable sweep wing, variable extension tail

Further development of automatic control system in UAV might be to provide the ability to adapt to aircraft configuration change due to damage or morphing mechanism. Development of a Mini-Morphing UAV (MiMo-UAV) is conducted to understand more about adaptive control system. The paper presents the design of the flying platform.

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