Practical active disturbance-rejection solution to a fly wing UAV flight control within full envelope

Engineering

• Unmanned Aerial Vehicle 100%
• Flight Control 100%
• Active Disturbance Rejection Control 100%
• Controller Design 66%
• Simulation Result 33%
• Parameter Uncertainty 33%
• Actuator 33%
• Engineering Application 33%
• Flight Envelope 33%
• High Aspect Ratio 33%
• Aerodynamic Characteristic 33%
• Reference Solution 33%
• Dynamic Process 33%
• Conventional Method 33%