A control system and method for a fully electric driven aircraft tractor

By using technical means such as adversarial perturbation generation adversarial network, quantum dynamic evolution neural network and feature refinement auto-coding neural network in the control system of all-electric drive aircraft tractors, the problems of weak data processing capabilities and low decision-making accuracy of existing systems are solved, and stronger data processing capabilities and higher decision-making accuracy are achieved.

CN119087822BActive Publication Date: 2025-03-25XIAN RVNUO NEW ENERGY
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Patent Information

Application Number
CN202411590058.6
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-11-08
Publication Date
2025-03-25
Estimated Expiration
2044-11-08

AI Technical Summary

Technical Problem

The data processing capability of the existing fully electric-driven aircraft tractor control system is weak, making it difficult to effectively process complex and high-dimensional driving data, resulting in poor feature extraction effect and loss of information or retaining irrelevant information during feature dimensionality reduction, thereby reducing decision-making accuracy.

Method used

The generative adversarial network algorithm based on adversarial perturbation is used to generate and expand driving data, combine the neural network algorithm with quantum dynamic evolution for feature extraction, and use the auto-encoded neural network based on feature refinement for feature dimensionality reduction. At the same time, an integrated gradient boosting tree algorithm based on dynamic decision boundaries is used in the tractor control module for classification decisions.

Benefits of technology

It significantly improves data processing capabilities and decision-making accuracy, can effectively capture important information in complex driving data, reduce the risk of information loss, and improve the generalization ability of the model and the ability to distinguish complex samples.

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Abstract

The present invention relates to the field of electrical digital data processing, and specifically to a full-electric drive aircraft tractor control system and method. The method mainly includes nine steps S1 to S9, and the system includes a data storage module, a data acquisition module, a data expansion module, a data processing module, a tractor control module, and an execution module. The existing full-electric drive aircraft tractor control system has the problems of weak data processing capability and low decision-making accuracy. The full-electric drive aircraft tractor control system and method provided by the present invention have strong data processing capability and high decision-making accuracy.
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