Adaptive Back-stepping Neural Control for an Embedded and Tiltable V-tail Morphing Aircraft

Engineering

• Nonlinear Model 100%
• Aerodynamics 50%
• Radial Basis Function 50%
• Simulation Result 50%
• Feedback Control 50%
• Degree of Freedom 50%
• External Disturbance 50%
• Aerodynamic Characteristic 50%
• First Order Filter 50%