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Application filed by Е.Г. ЖанжеровfiledCriticalЕ.Г. Жанжеров
Priority to SU4886297/22ApriorityCriticalpatent/SU1827987A1/en
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Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies
(AREA)
Abstract
FIELD: devices for stabilization of motion of flight vehicles. SUBSTANCE: device has sensor showing deviation of attitude of flying vehicle from programmed magnitude, analog-to-number converter, boosting member, number-analog converter, control actuator, first, second and third integrating units, first and second inverters, first and second signal sign separating units, displacement function determination unit and adder; device is also provided with 4th integrating unit and 3rd inverter connected in series; input of 3 rd inverter is connected with 2nd input of first signal sign separating unit; input of 4th integrating unit is connected with output of displacement function determination unit and its output is connected with second input of second integrating unit. EFFECT: improved dynamic characteristics of device. 3 dwg
SU4886297/22A1990-10-291990-10-29Device for attitude stabilization of flying vehicle
SU1827987A1
(en)
Feasibility study to develop a dc link VSCF system(Feasibility analysis of variable speed constant frequency inverter system using dc link approach for aircraft use)[Final Report]