Differentiator- and Observer-Based Feedback Linearized Advanced Nonlinear Control Strategies for an Unmanned Aerial Vehicle System

Engineering

• Actuator 20%
• Comparative Analysis 20%
• Control Design 20%
• Control Law 40%
• Control Strategy 100%
• Differentiator 100%
• Dynamic Models 20%
• Experimental Result 20%
• External Disturbance 20%
• Feedback Linearization 20%
• Metrics 20%
• Multiple-Input Multiple-Output 40%
• Nonlinearity 20%
• Observability 20%
• Rise Time 20%
• Rotor Speed 20%
• Rotors 40%
• Settling Time 20%
• Sliding Mode Control 100%
• State Feedback 20%
• Steady State Error 20%
• Systems Performance 20%
• Transients 20%
• Two Degree of Freedom 20%
• Unmanned Aerial Vehicle 100%
• Vehicle Dynamics 20%