The single system of gyro-verticals includes 3 central gyroscopic verticals TsGV-10P, installed on the shelf of the technical compartment:
- Left
- Right
- Control
The central vertical gyro TsGV-10P is designed to determine the spatial position of the aircraft.
TsGV is a two-gyro power stabilization system.
Communication TsGV-10P with aircraft.
TsGV-10P systems generate and transmit to consumers:
1) a signal proportional to the roll and pitch angles: - left CHV - into the main ACS channel, into the left pilot's checkpoint and into the main gyro unit GA-3 TKS-P; - CGV right - into the backup channel of the ACS, in the checkpoint of the right pilot and into the control gyro unit GA-3 TKS-P; - CGV control - on the roll and pitch indicator UKT-2, in the UVK, on the radar-P antenna, in DISS-013 and in the main gyro unit GA-3 in case of failure of the CGV left;
2) "READY" signal: - left and right main CHV - to the main and backup ACS channels; - TsGV control - in DISS-013
3) "FAILURE" signal: - left and right central gas supply voltages - to the "ARRETIR" lamps of the left and right checkpoint and in RI-65; - CHV control - on the board "FAILURE CHV KONTR." on the instrument panels of the left and right pilots and in the RI-65.
| Purpose | |
| Aircraft | IL-76, IL-78 |
| Onboard Systems | Unified vertical gyro system |

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