ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,4Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,4Follow0.74Rotor Torque (N·m)BTO-0.02960.17020.370.5698Jun 4, 2026Evaluation resultsMethodMethodLinksRotor Torque (N·m)Rotor Force (N)BTODrone Configuration=BTODrone Configuration=BTO2026.060.742.73UTODrone Configuration=UTODrone Configuration=UTO2026.060.221.29CCUDrone Configuration=CCUDrone Configuration=CCU2026.060—