Development of flight test platform for flapping wings micro air vehicles

• المؤلف الرئيسي: Pradipta, Johanes Eldwin
• مؤلفون آخرون: Lau Gih Keong
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2015
• الموضوعات: DRNTU::Engineering::Mechanical engineering::Machine design and construction
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/64582
• المؤسسة: Nanyang Technological University

This report presents the design, fabrication process, analysis and characterization of simple and low cost test platforms for force measurement of Flapping Wing Micro Air Vehicles (FWMAVs). Simple pendulum method and linearly guided load cell based test platforms currently used by the research group...