The invention belongs to a flight control system virtual test, and relates to a flight control system virtual test verification method based on a generative adversarial network, which comprises the following steps of: 1, acquiring flight control computer data from a flight control computer of an aircraft; 2, preprocessing the flight data of the flight control computer; 3, building a generative adversarial network model; 4, training the generative adversarial network model; 5, generating an enhanced data sample, and generating new data on the basis of the trained generative adversarial network model; according to the method, data enhancement is carried out on small sample flight control computer data, the sample size is enlarged, and the small sample problem is solved.

    本发明属于飞控系统虚拟试验,涉及基于生成式对抗网络的飞控系统虚拟试验验证方法,包括步骤:步骤1:从飞行器的飞控计算机中采集得到飞控计算机数据;步骤2:对飞控计算机的飞行数据进行预处理;步骤3:搭建生成式对抗网络模型;步骤4:训练生成式对抗网络模型;步骤5:生成增强数据样本,在训练好的生成式对抗网络模型模型基础上产生新数据;步骤6:静态、动态数据一致性验证,本发明的方法对小样本飞控计算机数据进行数据增强,扩大了样本量,解决了小样本问题。


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    Title :

    Flight control system virtual test verification method based on generative adversarial network


    Additional title:

    基于生成式对抗网络的飞控系统虚拟试验验证方法


    Contributors:
    CHEN YINCHAO (author) / WANG TAO (author) / YAN HONGYU (author) / ZHAO CHENGTAO (author) / XU MIN (author) / YE ZI (author)

    Publication date :

    2025-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen




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