ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,4,6Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,4,6Follow0Resultant Torque (N·m)BTO-0.001-0.000500.0005Jun 4, 2026Evaluation resultsMethodMethodLinksResultant Torque (N·m)Resultant Force (N)BTODrone Configuration=BTODrone Configuration=BTO2026.0600UTODrone Configuration=UTODrone Configuration=UTO2026.0600CCUDrone Configuration=CCUDrone Configuration=CCU2026.060—