ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,6Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,6Follow2.74Resultant Torque (N·m)BTO-0.10960.63021.372.1098Jun 4, 2026Evaluation resultsMethodMethodLinksResultant Torque (N·m)Resultant Force (N)BTODrone Configuration=BTODrone Configuration=BTO2026.062.7417.62UTODrone Configuration=UTODrone Configuration=UTO2026.062.3415.83CCUDrone Configuration=CCUDrone Configuration=CCU2026.060—