发明名称 СПОСОБ ОПРДЕЛЕНИЯ КОМПОНЕНТА СКОРОСТИ ЛЕТАТЕЛЬНОГО АППАРАТА
摘要 FIELD: physics. ^ SUBSTANCE: speed, flight-path speed and angle attitude of an aircraft are measured in flight. During post-flight processing of onboard measurement data the speed measurement reliability is defined. If reliability is positive the wind velocity is defined. Rated wind velocity is defined by its values at a given time or distance interval preceding the rate moment. To calculate the aircraft velocity components on the basis of flight-path speed and rated wind velocity the said given time or space interval includes also the next time or space interval after the rate moment. Rated wind velocity is calculated by regression for each rate moment. ^ EFFECT: improved precision of aircraft velocity components in all flight modes at random possible attack and grazing angles. ^ 5 dwg
申请公布号 RU2006119365(A) 申请公布日期 2007.12.27
申请号 RU20060119365 申请日期 2006.06.05
申请人 Открытое акционерное общество "ОКБ Сухого" (RU) 发明人 Собов Алексей Николаевич (RU);Р бошапка Виктор Григорьевич (RU);Варганов Андрей Владимирович (RU)
分类号 G01P5/00 主分类号 G01P5/00
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