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.


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    Titel :

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


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Yu, Xiang (Herausgeber:in) / Zhu, Hongyuan (Autor:in) / Liu, Xiaoxiong (Autor:in) / Zhang, YueHang (Autor:in) / Li, Yu (Autor:in)


    Erscheinungsdatum :

    2021-10-30


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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