System identification of aerodynamic derivatives for VTOL UAV

• المؤلف الرئيسي: Matiin Muhammad Hanifah Marican
• مؤلفون آخرون: Basman Elhadidi
• التنسيق: Final Year Project
• اللغة: English
• منشور في: Nanyang Technological University 2021
• الموضوعات: Engineering::Aeronautical engineering
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/150919

The establishment of an Aircraft Dynamic Model is a prerequisite to design navigation and control systems. However, aerodynamic models are not easily obtained for small- scaled aircraft model such as Unmanned Aerial Vehicles (UAVs) Simulated models are important towards the development of effective...