Control system development for unconventional aerobatic unmanned aerial vehicle with variable incidence wing

• المؤلف الرئيسي: Pham, Kim Hoan.
• مؤلفون آخرون: Go Tiauw Hiong
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2010
• الموضوعات: DRNTU::Engineering::Mechanical engineering::Control engineering; DRNTU::Engineering::Aeronautical engineering::Aircraft
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/40046
• المؤسسة: Nanyang Technological University

This final year project covers the design and development processes of control system for unconventional unmanned aerial vehicle (UAV). An aerobatic aircraft is designed to be equipped with variable incidence wing with an expectation to be able to perform both conventional aerobatic maneuvers as wel...