Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle

• المؤلف الرئيسي: Setiawan, Suhartono
• مؤلفون آخرون: Go Tiauw Hiong
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2009
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aircraft
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/19010

A ducted fan Vertical Take-off and Landing (VTOL) Micro Air Vehicle (MAV) is developed. The vehicle is equipped with a wing that can be rotated in the pitch direction (variable incidence). This feature is expected to suppress the altitude loss during transition and to reduce the gust effect in hover...