ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,2Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,2Follow2.91Rotor Torque (rT) [N · m]BTO-0.11640.66931.4552.2407Jun 4, 2026Evaluation resultsMethodMethodLinksRotor Torque (rT) [N · m]Rotor Force (rF) [N]BTODrone Configuration=BTODrone Configuration=BTO2026.062.9132.36UTODrone Configuration=UTODrone Configuration=UTO2026.062.7826.08CCUDrone Configuration=CCUDrone Configuration=CCU2026.060—