ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,3,6Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1,3,6Follow1.41Resultant Torque (N·m)BTO-0.05640.32430.7051.0857Jun 4, 2026Evaluation resultsMethodMethodLinksResultant Torque (N·m)Resultant Force (N)BTODrone Configuration=BTODrone Configuration=BTO2026.061.4115.92UTODrone Configuration=UTODrone Configuration=UTO2026.061.414.78CCUDrone Configuration=CCUDrone Configuration=CCU2026.060—