Availability: | |
---|---|
SG-1
SANGAS
SG-1 open-loop fiber optic gyroscope is used to measure the rotation angle rate of its mounting carrier relative to the inertial space.
It provides the rotating speed of the product along the sensitive axis of the carrier, which is mainly for the low precision demand of the flight control and servo control field.
Specifications | Performance | Unit |
Rate Range | 600 | deg/s |
Scale Factor(SF) | 3.2 | mV/deg/s |
Frequency range | 0... 1 | kHz |
Angle random walk | 0.03 | deg / h |
Bias stability, RMS | 10 | deg / h |
SF stability, RMS | 0.1 | % |
Readiness time | 0. 02 | s |
Temperature operating | -45 ... +70 | °C |
Endurance | -55... +85 | °C |
Vibration(operating), RMS | 13 | g |
Shocks(endurance) | 100 , 6 | g,ms |
MTBF | 50000 | hours (20 С, predicted) |
Lifetime(predicted) | 15 | year |
Dissipation | 1 | W |
Weight | 35 | gram |
Volume | 0.025 | litre |
Housing protection | Power coating | --- |
Tolerances | Per ISO 2768-m | ---- |
SG-1 open-loop fiber optic gyroscope is used to measure the rotation angle rate of its mounting carrier relative to the inertial space.
It provides the rotating speed of the product along the sensitive axis of the carrier, which is mainly for the low precision demand of the flight control and servo control field.
Specifications | Performance | Unit |
Rate Range | 600 | deg/s |
Scale Factor(SF) | 3.2 | mV/deg/s |
Frequency range | 0... 1 | kHz |
Angle random walk | 0.03 | deg / h |
Bias stability, RMS | 10 | deg / h |
SF stability, RMS | 0.1 | % |
Readiness time | 0. 02 | s |
Temperature operating | -45 ... +70 | °C |
Endurance | -55... +85 | °C |
Vibration(operating), RMS | 13 | g |
Shocks(endurance) | 100 , 6 | g,ms |
MTBF | 50000 | hours (20 С, predicted) |
Lifetime(predicted) | 15 | year |
Dissipation | 1 | W |
Weight | 35 | gram |
Volume | 0.025 | litre |
Housing protection | Power coating | --- |
Tolerances | Per ISO 2768-m | ---- |