FIELD: physics.
SUBSTANCE: proposed method comprises measuring aircraft flight parametres in transient conditions, automatic digital processing of measured parametres, and estimating aircraft flight mathematical model parametres, i.e. aerodynamic parametres of flight on variable-length in zero-overshoot base interval.
EFFECT: higher validity of aircraft flight mathematical model description and accuracy of estimating flight model parametres.
3 dwg
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Authors
Dates
2011-05-27—Published
2009-12-28—Filed