Aeroengine transient control has been analysed and one of the most important requirements for transient control is the safe and quick response to power request. Theoretically, the optimal operation is to follow the boundary of surge line (with surge margin) for acceleration while decreasing along burner blow-out limit for deceleration. However, in practice, surge and blow-out boundaries are extremely difficult to determine, particularly due to performance drift over flight envelope as well as engine usage cycle.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Optimization-Based Aeroengine Nonlinear Control Integration


    Contributors:

    Published in:

    Publication date :

    2021-08-18


    Size :

    38 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Model-Based Aeroengine Nonlinear Transient Control

    Wang, Jiqiang / Zhang, Weicun / Hu, Zhongzhi | Springer Verlag | 2021


    Aeroengine neural network control

    Tao, T. / Zhang, J. | British Library Online Contents | 1997


    Aeroengine and process of operating an aeroengine

    CARLOS HANNOVER GALINDO-LOPEZ | European Patent Office | 2025

    Free access


    Intelligent Performance Optimization Control of Aeroengine Based on Honey Badger Algorithm

    Liu, Zhidan / Gou, Linfeng / Chen, Yingxue et al. | IEEE | 2023