HIERARCHICAL GAIN SCHEDULING BASED TILT ANGLE GUIDED ROBUST CONTROL DURING MODE TRANSITION FOR TILT-ROTOR UNMANNED AIRCRAFT VEHICLE

Hierarchical gain scheduling based tilt angle guided robust control during mode transition for tilt-rotor unmanned aircraft vehicle

Tilt-rotor unmanned aircraft vehicle has the potential to combine vertical take-off and landing capability with efficient, high-speed cruise flight.However, the mode transition process is risky owing to the internal continuous time change of aerodynamic and external uncertain wind Accessories disturbances.Gain scheduling between two modes is common

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