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A fault-tolerant control method for quadrotor formation based on adaptive neural network

A neural network, fault-tolerant control technology, applied in the field of multi-agent systems

Active Publication Date: 2022-04-15
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Ordinary neural networks can obtain the weight matrix of the neural network through online or offline learning, but it is often difficult to analyze the stability of the system, while the adaptive neural network regards the weight matrix of the neural network as an adaptive variable, through The error information of the system updates the weight of the neural network. The adaptive neural network can not only realize the online self-learning of the neural network, but also ensure the stability of the system tracking error and the boundedness of the weight parameters of the neural network through the Lyapunov criterion. sex

Method used

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  • A fault-tolerant control method for quadrotor formation based on adaptive neural network
  • A fault-tolerant control method for quadrotor formation based on adaptive neural network
  • A fault-tolerant control method for quadrotor formation based on adaptive neural network

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[0122] And consider the failure of the actuator part of the first aircraft during the formation process, and the second and third aircraft have never failed during the operation. The time and size of the first aircraft's actuator failure are as follows:

[0123]

[0124] In order to verify the fault-tolerant control effect of the present invention, use the Simulink platform of MATLAB to carry out simulation verification, and the simulation results are as follows:

[0125] image 3 The tracking effect of the inner loop subsystem on the desired attitude is shown. Since the desired attitude angle given by the outer loop changes, there is a certain tracking error. Depend on Figure 3 It can be seen that the tracking error is small and the convergence speed is fast. In the case of partial failure of the actuator, the stability of the system and better control performance can still be guaranteed.

[0126] from Figure 4 , 5, 6, it can be seen that even in the case of the fail...

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Abstract

The invention discloses a four-rotor formation fault-tolerant control method based on an adaptive neural network. Aiming at a formation control system containing a plurality of four-rotor aircraft, the external interference that may occur in the system is considered, and the error information of the formation is used to design A quadrotor aircraft formation flight controller, using the neural network to compensate the loss caused by the failure, and using the Lyapunov stability theory to prove the stability, robustness and fault tolerance of the formation controller; based on the adaptive neural network control method , designed the attitude fault-tolerant controller of the inner loop of the quadrotor, which effectively improved the effect of attitude fault-tolerant control, and used the Lyapunov stability theory to prove that the system can still track the desired attitude in the case of actuator failure.

Description

technical field [0001] The invention relates to a four-rotor formation fault-tolerant control method based on an adaptive neural network, and belongs to the technical field of multi-agent systems. Background technique [0002] The quadrotor is a rotary-wing unmanned aircraft that can take off and land vertically. The basic structure of the quadrotor consists of a cross-shaped frame and four rotors mounted on the top of the frame. This special structure makes the control method of the quadrotor aircraft simpler and more convenient than other types of aircraft, and the attitude and position of the aircraft can be controlled by changing the rotation speed of the four rotors. The mutual coupling between the various control channels of the quadrotor aircraft is relatively weak and more flexible, so it has been widely used in power line patrol, SLAM, logistics transportation, aerial photography and other fields. [0003] With the rapid development of control theory and computer t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 张柯马人月姜斌陈谋盛守照甄子洋邵书义
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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