It can be applied to servo system, combined navigation, attitude reference system and other fields.
Strong vibration and shock resistance. It can provide accurate angular velocity information at -40°C~+85°C.
Using high-precision gyroscope and accelerometer. The accuracy of satellite combined navigation heading is superior0.3° (RMS). Control accuracy is better than 40urad.
Airships and other flight carriers, photoelectric pods (combined navigation and servo control), unmanned vehiclescars, turrets, robots, etc.
| Metric Category |
Metric Name |
Performance Metric |
Remarks |
|
Gyroscope parameters
|
measuring range |
±500°/s |
|
|
Scale factor repeatability |
< 50ppm |
|
|
|
Scale factor linearity |
<200ppm |
|
|
|
Biased stability |
<1°/h(1σ) |
National military standard | |
|
Biased instability |
<0.1°/h(1σ) |
Allan Curve |
|
|
Biased repeatability |
<0.5°/h(1σ) |
||
|
Bandwidth (-3dB) |
250Hz |
||
|
Accelerometer parameters |
measuring range |
±50g |
customizable |
|
Scale factor repeatability |
< 300ppm |
|
|
|
Scale factor linearity |
<1000ppm |
|
|
|
Biased stability |
<0.1mg(1σ) |
|
|
|
Biased repeatability |
<0.1mg(1σ) |
|
|
|
Bandwidth |
100HZ |
|
|
|
Interface Characteristics |
|||
|
Interface type |
RS-422 |
Baud rate |
921600bps (customizable) |
|
Data update rate |
1KHz(customizable) |
||
|
Environmental Adaptability |
|||
|
Operating temperature range |
-40°C~+85°C |
||
|
Storage temperature range |
-55°C~+100°C |
||
|
Vibration (g) |
6.06g (rms), 20Hz~2000Hz |
||
|
Electrical Characteristics |
|||
|
Input voltage (DC) |
+5V |
||
|
Physical Characteristics |
|||
|
Size |
44.8mm*38.5mm*21.5mm |
||
|
Weight |
55g |
||