Direct Force can eliminate the coupling between the force and moment, directly produce the force to change the trajectory of plane, it can improve carrier-based aircraft’s landing quality and efficiency. This paper will discuss the application of direct force and thrust vector technology based on F-16 aircraft model. Firstly, we discussed how thrust vector produce force and moment on airplane, and using thrust vector to apply direct force control on plane. Secondly, we design the dynamic inversion control and combine the control distribution technology to achieve inner loop control. Lastly, we design the direct lift model landing control law and the path angle rate model control law, the simulation results show that the path angle rate mode landing responses are more rapid.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Design of Carrier-Based Aircraft Landing Control Law Based on Direct Force


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Yu, Xiang (editor) / Zhu, Hongyuan (author) / Liu, Xiaoxiong (author) / Zhang, YueHang (author) / Li, Yu (author)


    Publication date :

    2021-10-30


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Design of Carrier-Based Aircraft Landing Control Law Based on Direct Force

    Zhu, Hongyuan / Liu, Xiaoxiong / Zhang, YueHang et al. | British Library Conference Proceedings | 2022


    Design of Carrier-Based Aircraft Landing Control Law Based on Direct Force

    Zhu, Hongyuan / Liu, Xiaoxiong / Zhang, YueHang et al. | TIBKAT | 2022


    Direct Lift Control Landing of Carrier-Based Aircraft Based on Preview Control

    Jie, Wang / Yang, Zhang / Ziyang, Zhen et al. | Springer Verlag | 2025


    RBFNN Adaptive Longitudinal Direct Lift Control of Carrier-Based Aircraft Landing

    Sun, Xiaoyun / Jiang, Ju / Zhen, Ziyang et al. | TIBKAT | 2022


    RBFNN Adaptive Longitudinal Direct Lift Control of Carrier-Based Aircraft Landing

    Sun, Xiaoyun / Jiang, Ju / Zhen, Ziyang et al. | Springer Verlag | 2021