A short landing run requirement for an aircraft is important from economic, operational and strategic considerations. Too strong a braking produces skid, which is an undesirable condition, while weak braking results in a long landing run. The shortest possible (optimal) landing run without any skidding requires a variable braking force to match the frictional force at all times. The maximum allowable braking force at any instant is a random variable as the ground-induced excitation and the frictional force between the wheel and the tyre are random in nature. In view of the time lag in the actuation of a servo system and its completion of the execution, a one-step prediction is employed to obtain the braking force required at a further instant. This brake management system has been tried on a simple aircraft model. The scheme is found to work well with the model.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Landing response of aircraft with optimal anti-skid braking


    Additional title:

    Landeverhalten eines Flugzeugs beim optimalen schlupffreien Bremsen


    Contributors:
    Yadav, D. (author) / Singh, C.V.K. (author)

    Published in:

    Publication date :

    1995


    Size :

    16 Seiten, 5 Bilder, 1 Tabelle, 35 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






    Anti-skid braking system based on vertical load of aircraft landing gear

    TONG YABIN / BU SHENPING / ZHANG JIAN et al. | European Patent Office | 2023

    Free access

    Anti-skid induced aircraft landing gear instability

    Gualdi, Stefania | Online Contents | 2008


    Anti-skid induced aircraft landing gear instability

    Gualdi, Stefania / Morandini, Marco / Ghiringhelli, Gian Luca | Elsevier | 2008