METHOD OF IDENTIFYING AIRCRAFT AERODYNAMIC CHARACTERISTICS BY TEST RESULTS

摘要

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