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)
Mathematical Models of Aircraft Lateral Motion in the Presence of Low-Frequency Gusts
1972
29 pages
Report
Keine Angabe
Englisch
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