Dictionnaire français - anglais

sciences - iate.europa.eu
1 control of an adaptive aircraft with a morphing input... Nomenclature G = gust velocity G0 = gust velocity amplitude H = gust gradient length K = gain vector pF = fuselage separation variable pW = wing separation variable pT = tail separation variable q = pitch rate R * = reference maneuver trajectory T = thrust output t = time U = control vector V = aircraft velocity X = state vector x = position z = altitude δE = input elevator angle γ = flight-path angle θ = pitch angle θB = tail boom angle θT = tail incidence angle θW = variable wing incidence angle σU = longitudinal noise standard deviation σW = vertical noise standard deviation I
général - core.ac.uk - PDF: enu.kz


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