Author(s): Wang B; Zhao H; Hu X; Shen Y; Li N;

In this study, an innovative adaptive sliding mode fault-tolerant control approach is developed for an over-actuated vertical takeoff and landing (VTOL) fixed-wing unmanned aerial vehicle (UAV) with the capability to suppress overestimation of adaptive parameters. This method is designed to effectively address model uncertainties and actuator faults witho ...

Article GUID: 41475926

Author(s): Yu Z, Zhang Y, Jiang B, Yu X, Fu J, Jin Y, Chai T

ISA Trans. 2020 Jul 09;: Authors: Yu Z, Zhang Y, Jiang B, Yu X, Fu J, Jin Y, Chai T

Article GUID: 32680604