SU330458A1 - COMPUTER DEVICE - Google Patents
COMPUTER DEVICEInfo
- Publication number
- SU330458A1 SU330458A1 SU1321067/24A SU1321067A SU330458A1 SU 330458 A1 SU330458 A1 SU 330458A1 SU 1321067/24 A SU1321067/24 A SU 1321067/24A SU 1321067 A SU1321067 A SU 1321067A SU 330458 A1 SU330458 A1 SU 330458A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- input
- adder
- aircraft
- block
- amplifying
- Prior art date
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Вычислительное устройство для управления боковым движением летательного аппарата при его стабилизации на заданной траектории, содержащее усилительные, дифференцирующий блоки и сумматор на выходе устройства, связанный непосредственно с блоком типа "насыщение" и через усилительный блок - с первым входом устройства, который подсоединен к датчику отклонения летательного аппарата от заданного курса, а ко второму входу устройства подключен датчик отклонения летательного аппарата от заданной траектории, отличающееся тем, что, с целью увеличения допустимых в диапазонах углов сноса и ошибок выставки заданного курса, на входе нелинейного блока включен второй сумматор, один вход которого через усилительное звено с инвертором соединен с первым входом устройства, а второй вход сумматора через другой усилительный блок связан со вторым входом устройства, через дифференцирующий блок соединенным с сумматором на выходе устройства.A computing device for controlling lateral movement of the aircraft during its stabilization on a given trajectory, containing amplifying, differentiating blocks and an adder at the output of the device, connected directly to the block of "saturation" type and through the amplifying block to the first input of the device, which is connected to the aircraft deviation sensor device from the specified course, and a sensor deviation of the aircraft from the specified path is connected to the second input of the device, characterized in that the admissions in a range of drift angles and exhibition errors of a given course, the second adder is connected to the input of the nonlinear unit, one input of which is connected to the first input of the device through an amplifier link, and the second input of the adder through another amplifying block is connected to the second input of the device unit connected to the adder at the output of the device.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1321067/24A SU330458A1 (en) | 1969-02-24 | 1969-02-24 | COMPUTER DEVICE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1321067/24A SU330458A1 (en) | 1969-02-24 | 1969-02-24 | COMPUTER DEVICE |
Publications (1)
Publication Number | Publication Date |
---|---|
SU330458A1 true SU330458A1 (en) | 2005-07-27 |
Family
ID=60514742
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1321067/24A SU330458A1 (en) | 1969-02-24 | 1969-02-24 | COMPUTER DEVICE |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU330458A1 (en) |
-
1969
- 1969-02-24 SU SU1321067/24A patent/SU330458A1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1527910A (en) | Burner control systems | |
BE611821A (en) | Device for degassing the return liquid in hydraulic regulating systems | |
FR1304490A (en) | Feedback amplifier device | |
SU330458A1 (en) | COMPUTER DEVICE | |
ATA548672A (en) | CONTROL CIRCUIT FOR DYNAMIC CONNECTION OF PERIPHERAL EQUIPMENT, E.G. INPUT AND OUTPUT DEVICE OR ADDITIONAL MEMORY WITH BUFFER REGISTER, WITH AN INTERNAL MEMORY | |
DK106050C (en) | Electro-optical device. | |
FR1378498A (en) | Electronic optical luminance amplifier | |
FR1127115A (en) | Improvements to piloting systems for land vehicles, in particular those for tracked vehicles | |
JPS5398762A (en) | Differential amplifier circuit | |
GB706494A (en) | Improvements in or relating to gyro-verticals | |
JPS5374447A (en) | Display device | |
SHUTTERLY | Utilization of real plane method of analysis to determine output time and autocorrelation functions for general nonlinear devices with general input | |
FR1412371A (en) | Slaving device and damping device particularly applicable to gyro-compasses | |
SU716402A1 (en) | CALCULATOR OF ALIGNMENT OF SYSTEM OF AUTOMATIC CONTROL OF AIRPLANE LANDING | |
DK104715C (en) | Process for increasing the stability of pesticides containing dimethyldichlorovinyl phosphate and finely divided silica. | |
NOHEL | Problems in qualitative behavior of solutions of nonlinear volterra equations(Global existence, boundedness and behavior of solutions to nonlinear volterra equations) | |
SU392659A1 (en) | AUTOMATIC DEVICE FOR STABILIZATION OF AIRCRAFT | |
FR1269616A (en) | System of air navigation control and selective bilateral links by discontinuous scans | |
GELIG | On the application of lyapunov's second method to the investigation of the stability of motion of nonlinear discontinuous systems(Application of liapunov method to investigation of stability of motion of nonlinear discontinuous systems- automatic control) | |
FR1357832A (en) | Device stabilizing the zero and canceling the drift of continuous signal amplifiers | |
BARBASHIN et al. | Method for stabilizing a third-order control system with a high amplification factor, also used to increase dynamic accuracy of a servosystem | |
BE608381A (en) | Device for reading the time in any part of the world. | |
ES398517A1 (en) | Improvements in an integrating electronic device. (Machine-translation by Google Translate, not legally binding) | |
CA610698A (en) | Switched and proportional transistor servo amplifier circuit | |
FR1168866A (en) | Reduction device, especially for agricultural tractors and similar applications |