Integrated guidance and nonlinear feedback control of underactuated unmanned aerial vehicles in SE(3)

Keyphrases

• Actuation Model 20%
• Bounded Inputs 20%
• Configuration Manifold 20%
• Coordinate Frames 20%
• Discrete-time Model 20%
• Dynamic Scheme 20%
• Fixed-wing Unmanned Aerial Vehicles 20%
• Guidance Algorithm 20%
• Integrated Guidance 100%
• Multi-rotor Unmanned Aerial Vehicle 20%
• Nonlinear Feedback Control 100%
• Overall Stability Analysis 20%
• Quadcopter Unmanned Aerial Vehicles 20%
• Single Degree of Freedom 20%
• Special Euclidean Group 20%
• Thrust Direction 20%
• Under-actuated 20%
• Underactuated Unmanned Aerial Vehicles 100%
• Underactuated Vehicle 80%
• Vehicle Dynamics 20%
• Vertical Takeoff 20%

Engineering

• Fixed Wings 20%
• Nonlinear Feedback 100%
• Thrust Direction 20%