$L_{1}$ ADAPTIVE CONTROL OF A DUAL-ROTOR TAIL-SITTER UNMANNED AERIAL VEHICLE WITH INPUT CONSTRAINTS DURING HOVER FLIGHT

$L_{1}$ Adaptive Control of a Dual-Rotor Tail-Sitter Unmanned Aerial Vehicle With Input Constraints During Hover Flight

The input constraints of control surfaces Essential Minerals may lead to saturations, which could limit the achievable performance or even cause instability of vertical take-off and landing (VTOL) tail-sitter unmanned aerial vehicle (UAV).To improve flight safety and attitude tracking performance, a novel L1 adaptive control architecture for attitu

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