FIELD: aviation.
SUBSTANCE: backup aircraft orientation system comprises a full pressure sensor, a static pressure sensor, a signal processing and conversion device, computer, spatial orientation module, liquid crystal display, operating mode control device, yaw detector, photosensor, device for compensation of systematic component of zero shift of inertial sensors of spatial orientation module, built-in control system, one-time commands device, selection device, inclination angle compensation module, connected in a certain way.
EFFECT: increasing reliability and manufacturability due to the ability to choose the installation location and compensate for the angle of inclination of the instrument panel.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| INTEGRATED SYSTEM OF REDUNDANT INSTRUMENTS | 2009 |
|
RU2386927C1 |
| INTEGRATED SYSTEM OF STANDBY DEVICES | 2019 |
|
RU2728731C1 |
| INTEGRATED BACKUP DEVICE SYSTEM | 2016 |
|
RU2635821C1 |
| INTEGRATED SYSTEM OF BACKUP INSTRUMENTS | 2016 |
|
RU2656954C1 |
| INTEGRATED SYSTEM OF BACKUP DEVICES | 2020 |
|
RU2790217C2 |
| INTEGRATED SYSTEM OF STANDBY DEVICES | 2018 |
|
RU2734278C2 |
| INTEGRATED SYSTEM OF BACKUP DEVICES | 2020 |
|
RU2780634C2 |
| INTEGRATED SYSTEM OF STANDBY DEVICES | 2019 |
|
RU2733326C1 |
| INTEGRATED SYSTEM OF STANDBY DEVICES | 2017 |
|
RU2690029C1 |
| INTEGRATED SYSTEM OF BACKUP DEVICES AND METHOD FOR CALIBRATING MAGNETIC FIELD SENSOR OF INTEGRATED SYSTEM OF BACKUP DEVICES | 2015 |
|
RU2593424C1 |
