Transitional flight equilibrium and performance study for the X-NMRL tail-sitter VTOL MAV

Engineering

• Aerodynamic Model 100%
• Aerodynamics 100%
• Angle-of-Attack 100%
• Control Design 50%
• Control Model 50%
• Control Surface 50%
• Dynamic Model 50%
• Flight Path Angle 50%
• Iteration Algorithm 50%
• Max 50%
• Micro Air Vehicle 100%
• Momentum Theory 50%
• Parameter Variation 50%
• Performance Analysis 50%
• Performance Parameter 100%
• Propeller 50%
• Slipstream 50%
• Supplied Power 50%
• Vehicle Design 50%
• Vehicle Dynamics 50%