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Optimal reliability design for over-actuated systems based on the MIT rule: Application to an octocopter helicopter testbed

Reliability EngineeringEngineeringAerial RoboticsAerospace EngineeringAir Vehicle SystemMechatronicsMechanical SystemsOctocopter HelicopterSystems EngineeringMit RuleFlying RobotRotor DynamicOptimal Reliability DesignFlight Control