ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_1Follow0Resultant Torque (N·m)CCU-0.17441.00282.183.3572Jun 4, 2026Evaluation resultsMethodMethodLinksResultant Torque (N·m)Resultant Force (N)CCUDrone Configuration=CCUDrone Configuration=CCU2026.060—UTODrone Configuration=UTODrone Configuration=UTO2026.064.1431.24BTODrone Configuration=BTODrone Configuration=BTO2026.064.3633.46