Path generation and control for unmanned multirotor vehicles using nonlinear dynamic inversion and pseudo control hedging

Keyphrases

• Path Generation 100%
• High Velocity 100%
• Multirotor Vehicle 100%
• Nonlinear Dynamic Inversion 100%
• Path Control 100%
• Pseudo-control Hedging 100%
• External Disturbances 50%
• Control Approach 50%
• Extra Degree of Freedom 50%
• State Estimation 50%
• Temporal Error 50%
• Quadrotor 50%
• Path-based 50%
• GPS Receiver 50%
• Path Following 50%
• Predefined Path 50%
• Experimental Flight 50%
• Trajectory Tracking 50%
• Path Following Control 50%
• Modeling Uncertainty 50%
• Actuator Saturation 50%
• Trajectory Controller 50%
• Interactive Process 50%
• Unit Quaternion 50%
• Disturbance Uncertainties 50%
• Low-cost Inertial Sensors 50%
• Yaw Rotation 50%
• Multi-rotor UAV 50%
• Parallel Transport Frame 50%
• Thrust Saturation 50%
• Quaternionic Curve 50%

Engineering

• Non-Linear Dynamic 100%
• Degree of Freedom 50%
• Unmanned Aerial Vehicle 50%
• Additional Degree 50%
• Inertial Sensor 50%
• Progression 50%
• Flight Test 50%
• External Disturbance 50%
• Parallel Transport 50%
• Reference Model 50%
• State Estimation 50%
• Global Positioning System 50%
• Quadcopter 50%
• Actuator 50%