SU1468258A1 - DEVICE FOR CONTROL OF THE HEIGHT OF THE FLIGHT OF THE PLANE - Google Patents
DEVICE FOR CONTROL OF THE HEIGHT OF THE FLIGHT OF THE PLANEInfo
- Publication number
- SU1468258A1 SU1468258A1 SU4218017/24A SU4218017A SU1468258A1 SU 1468258 A1 SU1468258 A1 SU 1468258A1 SU 4218017/24 A SU4218017/24 A SU 4218017/24A SU 4218017 A SU4218017 A SU 4218017A SU 1468258 A1 SU1468258 A1 SU 1468258A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- input
- output
- trigger
- counter
- control
- Prior art date
Links
Landscapes
- Radar Systems Or Details Thereof (AREA)
Abstract
Устройство для контроля высоты полета самолета, содержащее радиовысотомер, первый выход которого соединен с входом первого порогового элемента, блок памяти, выход которого соединен с входом одновибратора, выход которого подключен к первому управляющему входу блока памяти, второй пороговый элемент, триггер, источник питания, отличающееся тем, что, с целью повышения информативности, в него введены датчик положения шасси, первый и второй элементы И, счетчик, первый выход радиовысотомера соединен с входом второго порогового элемента, выходы первого и второго пороговых элементов соединены соответственно с первым и вторым входами первого элемента И, выход которого подключен к инверсному входу обнуления и информационному входу триггера, выход которого соединен с первым входом второго элемента И и входом управления счетчика, выход которого соединен с вторым входом второго элемента И, выход которого подключен к второму управляющему входу блока памяти, выход одновибратора соединен со счетным входом счетчика, выход датчика положения шасси соединен с третьим входом первого элемента И, второй выход радиовысотомера подключен к тактовому входу триггера, выход источника питания соединен с инверсным входом установки в единичное состояние триггера.Device for controlling the altitude of the aircraft, containing a radio altimeter, the first output of which is connected to the input of the first threshold element, a memory unit, the output of which is connected to the input of a one-shot, the output of which is connected to the first control input of the memory unit, the second threshold element, trigger, power source, different so that, in order to increase the information content, a chassis position sensor, the first and second elements I, the counter, the first output of the radio altimeter are connected to the input of the second threshold element, the outputs the first and second threshold elements are connected respectively to the first and second inputs of the first element I, the output of which is connected to the inverse zeroing input and the information input of the trigger, the output of which is connected to the first input of the second element I and the control input of the counter, the output of which is connected to the second input of the second element And, the output of which is connected to the second control input of the memory block, the output of the one-shot is connected to the counting input of the counter, the output of the chassis position sensor is connected to the third input of the first element The receiver And, the second output of the radio altimeter is connected to the trigger input of the trigger, the output of the power supply is connected to the inverse input of the installation in the unit state of the trigger.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU4218017/24A SU1468258A1 (en) | 1987-03-30 | 1987-03-30 | DEVICE FOR CONTROL OF THE HEIGHT OF THE FLIGHT OF THE PLANE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU4218017/24A SU1468258A1 (en) | 1987-03-30 | 1987-03-30 | DEVICE FOR CONTROL OF THE HEIGHT OF THE FLIGHT OF THE PLANE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU1468258A1 true SU1468258A1 (en) | 2005-06-10 |
Family
ID=60536525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU4218017/24A SU1468258A1 (en) | 1987-03-30 | 1987-03-30 | DEVICE FOR CONTROL OF THE HEIGHT OF THE FLIGHT OF THE PLANE |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU1468258A1 (en) |
-
1987
- 1987-03-30 SU SU4218017/24A patent/SU1468258A1/en active
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