基于鲁棒伺服思想的尾坐式飞行器悬停姿态控制

Engineering

• Unmanned Aerial Vehicle 100%
• Attitude Control 100%
• Delay Time 100%
• Servomechanism 100%
• Control System 50%
• Aerodynamics 50%
• Performance Degradation 50%
• Simulation Result 50%
• Flight Test 50%
• Moment of Inertia 50%
• Dynamic Model 50%
• Limited Performance 50%
• Extended State Observer 50%
• Good Performance 50%
• Adaptive Controller 50%
• Equilibrium Point 50%
• Actuator Failure 50%
• Controller Parameter 50%
• Kinematic Model 50%