The automatic carrier landing process is a significant and complex due to the plant variation of carrier-based aircraft. To reasonably identify the stability interval for specific performance, an adaptive control strategy based on the guardian map approach is proposed. Prescribed performance, namely, stability margin, damping requirements, or flying quality requirements, is analytically formulated using a guardian map. The null space of guardian maps restricts the prescribed performance regarding the poles’ location. The feasible corridor of control parameters is generated based on the null space of guardian maps. Besides, a velocity-adaptive prescribed performance control method is proposed to conduct the attitude control of carrier-based aircraft. Simulation shows that the short-period mode of carrier-based aircraft will be driven from unstable to stable as the velocity decreases. Moreover, simulation results demonstrate the proposed control method and indicate that the attitude loop control of carrier-based aircraft possesses more underdamped responses as the velocity decreases.


    Access

    Download


    Export, share and cite



    Title :

    Velocity-Adaptive Prescribed Performance Control for Carrier-Based Aircraft Based on Guardian Maps


    Contributors:
    Chenliang Li (author) / Jizhou Lai (author) / Boyi Chen (author) / Yanbin Liu (author)


    Publication date :

    2023




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Adaptive control of hypersonic vehicles using guardian maps theory

    Mengying, Liu / Zhiyong, She / Dibo, Xiao et al. | IEEE | 2015




    Longitudinal Flight Control Synthesis with Guardian Maps

    Saussie, D. / Akhrif, O. / Berard, C. et al. | British Library Conference Proceedings | 2009


    Application of guardian maps theory in flight control system design for aircraft model

    Liu, Yanbin / Li, Chenliang / Liu, Mengying et al. | IEEE | 2014