Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity

Engineering

• Adaptive Control 50%
• Boundedness 50%
• Control Surface 100%
• Feedback Control 50%
• Flexible Couplings 50%
• Flight Path Angle 50%
• Functional Decomposition 50%
• Gain Function 100%
• Hypersonic Flight Vehicle 100%
• Nonlinearity 100%
• Pitch Angle 50%
• Rigid Structure 50%
• Robust Design 50%
• Simulation Result 50%
• Singularities 50%