According to the needs of flight, based on the automatic control technology, the steering gear and the vertical gyroscope are used to realize the sliding approach, free elevation and attitude maintenance, and the structured design of the shoe-type aircraft. The fine adjustment of the rising rudder angle and the different rotation force of the pitch angle can carry out error tracking, realize the stable adjustment of different states, and also achieve the purpose of rapid response. The accuracy of the cooperation between the two boots also depends on the optimization strategy of the system and the control of the rising threshold. The deficiencies in the initial setting model can be adjusted through the advanced filtering and lagging network correction of the model to achieve the precise service of the system And seamless cooperation. This article gives the automatic control design steps and optimized paths for precise adjustment.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Research on Modular Cooperative Optimal Control of Low Altitude Approach Booted Aircraft


    Contributors:
    Li, Jiusheng (author) / Kong, Depeng (author) / Dai, Shaoqing (author) / Gu, Weisi (author) / Chen, Xinyue (author) / Kong, Dehui (author)


    Publication date :

    2021-10-20


    Size :

    1140621 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Suited and booted: new suits in demand

    British Library Online Contents | 2005



    Flight and ground tests of a laser-booted vehicle

    Mead, Jr., Franklin / Myrabo, Leik / Messitt, Donald | AIAA | 1998



    Biomechanical Response of Military Booted and Unbooted Foot-Ankle-Tibia from Vertical Loading

    Merkle, Andrew C. / Pintar, Frank A. / Voo, Liming et al. | SAE Technical Papers | 2016