Adaptive control of unmanned aerial vehicles: Theory and flight tests

Keyphrases

• Adaptive Control 100%
• UAV 100%
• Adaptive Element 100%
• Vehicle Theory 100%
• Inverse Model 66%
• Scale Model 33%
• Helicopter 33%
• Degrees of Freedom 33%
• Actuator 33%
• Outer Loop 33%
• Closed-loop System 33%
• Translational Motion 33%
• Six Degrees of Freedom 33%
• Approximate Inverse 33%
• Feedback Linearization 33%
• Angular Velocity 33%
• Adaptive Controller 33%
• Control Input 33%
• Adaptive Control Design 33%
• Flight Control 33%
• Flight Envelope 33%
• Long-term Retention 33%
• Angular Rate 33%
• Vehicle Attitude 33%
• Fixed-wing UAV 33%
• Adaptive Control System 33%
• Body Axis 33%
• Underactuated System 33%
• Fully-actuated 33%
• Vehicle Position 33%
• Flight Control Algorithm 33%
• Inversion Errors 33%
• Track Position 33%
• Roll-pitch 33%
• Ducted Fan 33%
• Rotor UAV 33%
• Fixed-wing Aircraft 33%
• UAV Helicopter 33%
• Actuator Rate Saturation 33%
• Uncertainty Approximation 33%
• Thrust Vector 33%
• Saturation Element 33%
• Nonlinear Reference Models 33%
• Actuator Magnitude Saturation 33%

Engineering

• Unmanned Aerial Vehicle 100%
• Adaptive Control 100%
• Flight Test 100%
• Degree of Freedom 50%
• Flight Control 50%
• Fixed Wings 50%
• Controllability 25%
• Control Algorithm 25%
• Rotorcraft 25%
• Feedback Control System 25%
• Control Design 25%
• Reference Model 25%
• Angular Velocity ω 25%
• Feedback Linearization 25%
• Adaptive Controller 25%
• Control Input 25%
• Scale Model 25%
• Flight Envelope 25%
• Outer Loop 25%
• Desired Position 25%
• Underactuated System 25%
• Ducted Fan 25%
• Roll Axis 25%
• Command Trajectory 25%