ResearchBenchmarksStructural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_0Structural Controllability Analysis on Hexacopter Rotor Fault Scenarios Condition Lambda_0Follow8.42Rotor Torque (N · m)BTO0.12.264.426.58Jun 4, 2026Evaluation resultsMethodMethodLinksRotor Torque (N · m)Rotor Force (N)BTODrone Configuration=BTODrone Configuration=BTO2026.068.4263.92UTODrone Configuration=UTODrone Configuration=UTO2026.068.1755.17CCUDrone Configuration=CCUDrone Configuration=CCU2026.060.42—