ADAPTIVE FILTRATION SYSTEM FOR AERODYNAMIC ANGLES OF AIRCRAFT

FIELD: measurement technology.SUBSTANCE: group of inventions relates to device, system and method of recording aerodynamic angles. Method is realized to calculate first and second aerodynamic angles variation rates, filtered aerodynamic angle is calculated to control aircraft in steady gust.EFFECT:...

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1. Verfasser:	LO Tszya
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CALCULATING COMPUTING CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS COUNTING ELECTRIC DIGITAL DATA PROCESSING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS HELICOPTERS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: measurement technology.SUBSTANCE: group of inventions relates to device, system and method of recording aerodynamic angles. Method is realized to calculate first and second aerodynamic angles variation rates, filtered aerodynamic angle is calculated to control aircraft in steady gust.EFFECT: disclosed is an adaptive filtration system for aerodynamic angles of an aircraft.18 cl, 13 dwg Группа изобретений относится к устройству, системе и способу регистрации аэродинамических углов. Для реализации способа вычисляют первою и вторую скорости изменения аэродинамических углов, вычисляют отфильтрованный аэродинамический угол для возможности управления летательным аппаратом при устойчивом порыве ветра. 3 н. и 15 з.п. ф-лы, 13 ил.