Aerodynamics-Driven Morphing Control and Flight Test for Compound Flexible Multibody Aircraft

Engineering

• Aerodynamics 100%
• Flight Test 100%
• Reconfiguration 50%
• Degree of Freedom 50%
• Dynamic Model 50%
• Adaptability 50%
• Control Structure 50%
• Aerodynamic Efficiency 50%
• Multibody Dynamics 50%
• Wingtips 50%
• Aerodynamic Surface 50%