FIELD: measurement.
SUBSTANCE: invention relates to measurement and indication systems, which provide for piloting of aircraft in case of failure of main flight-navigation systems. Integrated system of backup devices includes a full pressure sensor, a static pressure sensor, a signal processing and conversion device, a computer, a spatial orientation module, a liquid crystal display, braking sensor, operating mode control device, car transceiver, photosensor, device for compensation of systematic component zero displacement of inertial sensors of spatial orientation module, measuring resistor, built-in control system, current stabilizer, commutator, ADC, reference voltage source, braking device control device.
EFFECT: higher safety of piloting of aircraft and reliability of system.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| INTEGRATED SYSTEM OF REDUNDANT INSTRUMENTS | 2009 |
|
RU2386927C1 |
| INTEGRATED SYSTEM OF BACKUP DEVICES | 2020 |
|
RU2780634C2 |
| INTEGRATED SYSTEM OF BACKUP DEVICES | 2020 |
|
RU2790217C2 |
| INTEGRATED SYSTEM OF STANDBY DEVICES | 2019 |
|
RU2733326C1 |
| INTEGRATED BACKUP DEVICE SYSTEM | 2016 |
|
RU2635821C1 |
| INTEGRATED SYSTEM OF STANDBY DEVICES | 2017 |
|
RU2690029C1 |
| INTEGRATED SYSTEM OF STANDBY DEVICES | 2018 |
|
RU2734278C2 |
| BACKUP ORIENTATION SYSTEM | 2023 |
|
RU2826174C1 |
| INTEGRATED SYSTEM OF BACKUP INSTRUMENTS | 2016 |
|
RU2656954C1 |
| AIRPLANE AND HELICOPTER INTEGRATED STANDBY EQUIPMENT SYSTEM | 2006 |
|
RU2337315C2 |
