The invention relates to the technical field of multi-unmanned aerial vehicle formation
fault tolerance, in particular to a multi-unmanned aerial vehicle formation adaptive fuzzy sliding mode
fault tolerance control method, which comprises the steps of S1, establishing a multi-unmanned aerial vehicle formation
system dynamic model; s2, defining a formation global
position tracking error and a speed
tracking error based on a navigation-following architecture and a communication topological structure; s3, designing a disturbance interval observer, and estimating upper and lower bounds of unknown external disturbance in real time by establishing a disturbance exogenous model and an auxiliary variable adaptive law; s4, constructing an
integral sliding mode surface based on a preset
performance function, performing adaptive approximation on the lumped uncertain item by adopting a
fuzzy logic system, and designing an adaptive fuzzy sliding mode fault-tolerant controller; and S5, proving that the formation
tracking error is gradually converged to zero in
finite time through
Lyapunov stability analysis. When the unmanned aerial vehicle breaks down,
reliable transmission of task information and formation keeping can be guaranteed, good robustness and environmental adaptability are achieved, and the stable control performance of the unmanned aerial vehicle in a complex task scene is effectively improved.