Model-Based Optimization Approach for PID Control of Pitch-Roll UAV Orientation

Engineering

• Derivative Controller 100%
• Proportional-Integral-Derivative Control 100%
• Unmanned Aerial Vehicle 100%
• Optimization Approach 100%
• Absolute Error 100%
• Rotors 50%
• Drone 50%
• Control Model 50%
• Internal Model Control 50%
• Multiobjective Approach 50%
• Error Form 50%
• Roll Angle φ 50%
• Controller Design 50%
• Cost Function 50%
• Nonlinear Model 50%
• Design Phase 50%

Keyphrases

• Model Optimization 100%
• UAV 100%
• Proportional-integral-derivative Controller 100%
• Optimization Approach 100%
• Vehicle Orientation 100%
• Controller Design 25%
• Nonlinear Model 25%
• Platform Trials 25%
• Control Model 25%
• Optimization Control 25%
• Design Phase 25%
• Model-based Approach 25%
• Internal Model Control 25%
• Integral Absolute Error 25%
• Angle Orientation 25%
• Control Challenges 25%
• Roll Angle 25%
• Battery Consumption 25%
• Weighted Cost Function 25%
• Drone System 25%
• Simulink 25%
• Quadrotor Unmanned Aerial Vehicle 25%
• Integral Time Absolute Error 25%
• Multi-objective Approach 25%