SU365689A1 - SIDE MOTION CONTROL SYSTEM OF THE AIRCRAFT - Google Patents
SIDE MOTION CONTROL SYSTEM OF THE AIRCRAFTInfo
- Publication number
- SU365689A1 SU365689A1 SU1086296/24A SU1086296A SU365689A1 SU 365689 A1 SU365689 A1 SU 365689A1 SU 1086296/24 A SU1086296/24 A SU 1086296/24A SU 1086296 A SU1086296 A SU 1086296A SU 365689 A1 SU365689 A1 SU 365689A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- roll
- given
- aircraft
- control system
- motion control
- Prior art date
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Система управления боковым движением летательного аппарата, содержащая датчики крена и отклонения от заданного курса и заданной траектории, блок, формирующий сигнал заданного крена, отличающаяся тем, что, с целью повышения точности управления, в ней дополнительно установлены изодромное, апериодическое и инвертирующее звенья, причем выход датчика отклонения от заданного курса через изодромное звено, а выход датчика крена через последовательно соединенные инвертирующее и апериодическое звенья подключены ко входу блока, формирующего сигнал заданного крена.The control system of the lateral movement of the aircraft, containing sensors roll and deviations from a given course and a given trajectory, a unit that generates a signal of a given roll, characterized in that, in order to improve control accuracy, it additionally installed an isodromic, aperiodic and inverting links, and the output sensor deviations from the set course through the isodromic link, and the output of the roll sensor through the series-connected inverting and aperiodic links are connected to the input of the block forming the sy drove a given roll.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1086296/24A SU365689A1 (en) | 1966-07-05 | 1966-07-05 | SIDE MOTION CONTROL SYSTEM OF THE AIRCRAFT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1086296/24A SU365689A1 (en) | 1966-07-05 | 1966-07-05 | SIDE MOTION CONTROL SYSTEM OF THE AIRCRAFT |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU833646253A Addition SU1170221A2 (en) | 1983-09-27 | 1983-09-27 | Boiler unit |
Publications (1)
Publication Number | Publication Date |
---|---|
SU365689A1 true SU365689A1 (en) | 2005-07-27 |
Family
ID=60514824
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1086296/24A SU365689A1 (en) | 1966-07-05 | 1966-07-05 | SIDE MOTION CONTROL SYSTEM OF THE AIRCRAFT |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU365689A1 (en) |
-
1966
- 1966-07-05 SU SU1086296/24A patent/SU365689A1/en active
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