It is civil aviation inertial navigation system standards of the new generation of navigation systems and it can effectively protect the flight safety and transport efficiency.
Attributes |
Index |
Heading |
|
Range |
±180° |
Accuracy |
< 2° |
Resolution |
0.01° |
Attitude |
|
Range: Roll, pitch |
±180° |
Dynamic Accuracy |
<0.3° |
|
0.01° |
Angular velocity |
|
Range: roll, pitch, yaw |
±300°(±900°) |
Zero absolute error |
< 0.15deg/s(< 0.02deg/s) |
Zero - point instability |
6° |
Resolution |
0.01° |
ARW |
< 0.15° |
Acceleration |
|
Range |
±6g |
Bias stability |
< 5mg |
Resolution |
< 1mg |
working environment |
|
|
100g@6ms |
Non-power shock |
10000g@6ms |
Anti-seismic |
6g rms |
Operating temperature |
-40°—85° |
Electrical interface |
|
Input voltage |
5-13V |
Size |
84 x 60 x 35mm |
Weight |
50g |
Interface Type |
10Pin |