ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,2,4Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,2,4Follow0.18Rotor Torque (N·m)BTO-0.00720.04140.090.1386Jun 4, 2026Evaluation resultsMethodMethodLinksRotor Torque (N·m)Rotor Force (N)BTODrone Configuration=BTODrone Configuration=BTO2026.060.180.74UTODrone Configuration=UTODrone Configuration=UTO2026.060.050.6CCUDrone Configuration=CCUDrone Configuration=CCU2026.060—