SU295516A1 - COMPUTING DEVICE FOR AIRCRAFT CONTROL - Google Patents
COMPUTING DEVICE FOR AIRCRAFT CONTROLInfo
- 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
Links
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.
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) |
-
1969
- 1969-09-29 SU SU1362194/24A patent/SU295516A1/en active
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