Finite-time terminal sliding mode attitude control for tailless full-wing configuration UAVs based on extended state observers and auxiliary compensators

Engineering

• Unmanned Aerial Vehicle 100%
• Attitude Control 100%
• Sliding Mode Controller 100%
• Sliding Mode 100%
• Finite Time 100%
• Extended State Observer 100%
• Nonlinearity 66%
• Convergence Time 33%
• Convergence Speed 33%
• Flight Envelope 33%
• Control Parameter 33%
• Sliding Surface 33%
• Attitude Angle 33%
• Initial State 33%
• Control Command 33%
• Rotational 33%
• Angular Velocity ω 33%
• Propeller 33%
• Outer Loop 33%
• Euclidean Norm 33%