Results of aircraft lateral motion in the presence of gases are presented in order to investigate the effects of low altitude gases upon performance during a fully automatic aircraft landing approach. A brief description is given of the approximations and properties of the random, three-dimensional gust velocity fields in terms of stationarity, homogeneity, and isotropy. Particularly a set of linear differential equations are derived which describe approximately aircraft lateral motion and control in the presence of low-frequency gusts, the aircraft being a large passenger-transport type with a roll control. (Author)


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    Title :

    Mathematical Models of Aircraft Lateral Motion in the Presence of Low-Frequency Gusts


    Contributors:

    Publication date :

    1972


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English