PSD INDI and wake gradient based control of high aspect ratio UAVs' close formation flight

Engineering

• Unmanned Aerial Vehicle 100%
• Non-Linear Dynamics 100%
• High Aspect Ratio 100%
• Control Loop 66%
• State Estimation 33%
• Vortex 33%
• Estimation Error 33%
• Attitude Control 33%
• Flight Control 33%
• Feedforward 33%
• Relative Position 33%
• Extended State Observer 33%
• Flight Dynamics 33%
• Sudden Change 33%
• Propeller 33%
• Flight Safety 33%
• Angular Acceleration 33%
• Longitudinal Stability 33%
• Directional Stability 33%
• Lateral Force 33%