The inertial measurement unit (hereinafter referred to as the ‘product’) uses a three-axis integrated fiber optic gyroscope and a three-axis MEMS accelerometer as sensitive devices for angular velocity and visual acceleration, respectively, to measure the angular velocity and acceleration information of each axis of the carrier coordinate system. The angular velocity and acceleration information are sent to the acquisition and processing circuit, and after sampling, filtering, and error compensation, the angular velocity and visual acceleration information are output to the outside world.
The product has high precision, small size, light weight, and strong adaptability, suitable for attitude control and inertial navigation. It can be widely used in fields such as autonomous driving, unmanned aerial vehicles, electro-optical pods, submersibles, and missile navigation systems.
Part No, :
UF600Order(MOQ) :
11. Product specification
No. |
Content |
Index |
|
Performance indicators of gyroscope |
|||
1 |
Zero bias indicator |
Full temperature zero bias stability (10s, 1 σ) |
≤0.2°/h |
2 |
Full temperature zero bias repeatability |
≤0.2°/h |
|
3 |
Scale factor |
Scale factor nonlinearity |
≤100ppm |
4 |
Scale factor repeatability |
≤100ppm |
|
5 |
Other indicators |
Random walk |
≤0.05°/ |
6 |
Measuring range |
±900°/s |
|
Performance indicators of accelerometer |
|||
7 |
Range |
Measuring range |
±50g |
8 |
Zero bias indicator |
(10s, 1σ) |
≤200ug |
9 |
Zero bias repeatability |
≤200ug |
|
10 |
scale factor |
Scale factor repeatability (ppm) |
≤100ug |
Other performance indicators |
|||
11 |
Other indicators |
Supply voltage |
+5V±0.25V |
12 |
Power consumption |
≤6W |
|
13 |
Operation temperature |
-40℃~+70℃ |
|
14 |
Data output rate |
≥1000Hz |
|
15 |
Weight |
<350g |
|
16 |
Electrical interface |
1-channel RS422 |
|
17 |
External dimensions |
63mm×63mm×53mm |
2. Product dimension
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