Perching aircraft dynamics and control optimization

• المؤلف الرئيسي: Mau, Zao Min.
• مؤلفون آخرون: Go Tiauw Hiong
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2009
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aerodynamics
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/16202
• المؤسسة: Nanyang Technological University

This final year project covers the optimization of aircraft perching maneuver through geometric reconfiguration or morphing. A novel Unmanned Aerial Vehicle (UAV) model which adopts canard configuration and variable-incidence outer wings is specially designed for the analysis of perching maneuver. A...