FIELD: transport.
SUBSTANCE: method relates to aircraft engineering. Proposed method comprises generating module of observations on the base of aircraft nonlinear model that describes aircraft motion for all six degrees of freedom (DoF) and flexible motion of aircraft airframe, continuous feed of all data and measurement results significant for description of aircraft state in observation module, and calculating gust velocities and loads on airframe with the help of observation module proceeding from input data and measurement results.
EFFECT: higher safety standards, reduced costs and time-on-airfield.
49 cl, 40 dwg
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