The paper concentrates on the problem of fault-tolerant control of UAV against actuator faults from the perspective of flight control system architecture. Using backstepping control method and inverse optimization theory. the design of backstepping optimal control law was constructed. Based on the fault monitoring mechanism of vehicle management computer in the distributed flight cont... https://www.roneverhart.com/Ultimate-Support-LIVE-T-Standard-Height-One-Hand-Mic-Stand-with-Tripod-Base/