The invention relates to the technical field of aerocar
mode switching, and discloses a distributed driving aerocar self-adaptive fault-tolerant control method for
actuator multimode failure, which comprises the following steps: constructing a unified six-degree-of-freedom dual-mode
state space model; residual signals are generated based on extended Kalman filtering and a sliding-mode observer, and fault types and positions are positioned in real time through a lightweight classifier; the method comprises the following steps: extracting residual time-frequency features, identifying hard faults by using a lightweight
convolutional neural network, quantifying soft fault degrees through an incremental
support vector machine, fusing multi-source information based on a
Bayesian network to output fault types, levels and confidence coefficients, and introducing an
incremental learning mechanism to realize self-evolution of a diagnosis model; a
virtual control instruction is generated by adopting hierarchical
sliding mode control, thrust and
torque distribution of remaining actuators is optimized based on a dynamic quadratic
programming algorithm,
control parameters are adjusted online in combination with a Lyapunov adaptive law, aerodynamic interference and model uncertainty are inhibited,
attitude stability and trajectory tracking in air-ground
mode switching are guaranteed, and the method has the advantages of being high in reliability and high in reliability. And the fault-tolerant performance and the
operation safety of the hovercar in the air-ground
mode switching process are obviously enhanced.