Active disturbance rejection attitude control for the dove flapping wing micro air vehicle in intermittent flapping and gliding flight

Engineering

• Active Disturbance Rejection Control 66%
• Attitude Control 100%
• Closed Loop 33%
• Control Scheme 33%
• Control Strategy 33%
• Differentiator 66%
• Extended State Observer 66%
• Feedback Control 33%
• Feedback Controller 33%
• Micro Air Vehicle 100%
• Nonlinearity 33%
• Observer Gain 33%
• Reduce Energy Consumption 33%
• State Error 33%
• System State 33%