SU295516A1 - COMPUTING DEVICE FOR AIRCRAFT CONTROL - Google Patents

COMPUTING DEVICE FOR AIRCRAFT CONTROL

Info

Publication number
SU295516A1
SU295516A1 SU1362194/24A SU1362194A SU295516A1 SU 295516 A1 SU295516 A1 SU 295516A1 SU 1362194/24 A SU1362194/24 A SU 1362194/24A SU 1362194 A SU1362194 A SU 1362194A SU 295516 A1 SU295516 A1 SU 295516A1
Authority
SU
USSR - Soviet Union
Prior art keywords
computing device
deviation
angle
flight path
limiter
Prior art date
Application number
SU1362194/24A
Other languages
Russian (ru)
Inventor
С.В. Зеленков
Ф.А. Фурман
А.И. Брук
Л.Д. Брыкова
А.Ф. Маслова
Л.Л. Николаев
Ф.М. Педь
Ю.С. Розенфельд
Original Assignee
С.В. Зеленков
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by С.В. Зеленков filed Critical С.В. Зеленков
Priority to SU1362194/24A priority Critical patent/SU295516A1/en
Application granted granted Critical
Publication of SU295516A1 publication Critical patent/SU295516A1/en

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Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Вычислительное устройство для управления самолетом, содержащее операционный усилитель с обратной связью и выходным ограничителем, апериодическое звено, ограничитель сигнала вычислительного устройства и датчики угла отклонения от заданного курса полета и от заданной траектории полета, отличающееся тем, что, с целью увеличения точности управления самолетом, ко входу ограничителя сигнала вычислительного устройства подключен датчик угла отклонения от заданного курса полета и выход апериодического звена, ко входу которого подсоединен выходной ограничитель операционного усилителя, подключенного к датчику угла отклонения от заданной траектории полета, а звено отрицательной обратной связи операционного усилителя выполнено в виде Т-образного RC-фильтра, в плечах которого - два резистора, а в диагонали - последовательно соединенные резистор и конденсатор, причем их общая точка подключена через резистор к датчику угла отклонения от заданного курса полета.Computing device for aircraft control, containing an operational amplifier with feedback and output limiter, aperiodic link, signal limiter of the computing device, and sensors of deviation angle from a given flight path and from a given flight trajectory, characterized in that the input limiter signal of the computing device is connected to the sensor of the angle of deviation from a given flight path and the output of the aperiodic link, to the input of which is connected to The output limiter of the operational amplifier connected to the sensor of the angle of deviation from the specified flight path, and the negative feedback link of the operational amplifier is made in the form of a T-shaped RC filter, in the arms of which there are two resistors and in the diagonal series-connected resistor and capacitor their common point is connected through a resistor to the sensor of the angle of deviation from a given flight path.

SU1362194/24A 1969-09-29 1969-09-29 COMPUTING DEVICE FOR AIRCRAFT CONTROL SU295516A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1362194/24A SU295516A1 (en) 1969-09-29 1969-09-29 COMPUTING DEVICE FOR AIRCRAFT CONTROL

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1362194/24A SU295516A1 (en) 1969-09-29 1969-09-29 COMPUTING DEVICE FOR AIRCRAFT CONTROL

Publications (1)

Publication Number Publication Date
SU295516A1 true SU295516A1 (en) 2005-07-27

Family

ID=60514269

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1362194/24A SU295516A1 (en) 1969-09-29 1969-09-29 COMPUTING DEVICE FOR AIRCRAFT CONTROL

Country Status (1)

Country Link
SU (1) SU295516A1 (en)

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