MEMS Inertial Navigation System Industrial Inertial Measurement System Module Level MM-5322

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xProduct Name | Inertial Navigation System | Grade | Industrial |
---|---|---|---|
Applications | Aerospace, Defense, Navigation, Robotics | Customized Support | OEM, ODM |
Frequency | BDS B1I/B2I/B3I , GPS L1/L2/L5 GLONASS L1/L2 , GALILEO E1//E5a/E5b | GNSS Effective | 0.03m/s |
Highlight | MEMS Inertial Navigation System,Inertial Navigation System Industrial,Inertial Measurement System Module Level |
MM-5322 Module-Level MEMS Integrated Navigation System
MM-5322 is a module-level MEMS integrated navigation system with built-in MEMS IMU (inertial measurement unit) and high-precision dual-antenna GNSS . It adopts multi-source fusion Kalman filter algorithm and can provide continuous and reliable high-precision positioning and navigation information in complex environments. The products are widely used in satellite communications, drones, surveying and mapping, intelligent driving and other fields.
Key Features:
Support BDS , GPS , GLONASS , Galileo and QZSS full system multi-frequency points, support Beidou three satellite systems
Adaptive static / dynamic alignment
System-level installation error and wheel speed proportional error adaptive compensation
LVTTL , CAN , PPS , EVENT interfaces are available
High reliability product design, scientific and effective product development Professional and complete production equipment, strict quality control production process Deliver better products to users.Many years of industry application experience and practical cases of over a thousand industry users Industry-leading compensation calibration technology, efficient and fast professional technical response Provide users with more satisfactory services
Specifications:
Indicator |
Specifications (typical values) |
Remark |
|
Startup time |
Integrated navigation alignment time |
<60s |
Dual antenna, wide |
|
|||
Including GNSS cold start 25s , RTK initialization 5s |
|||
Satellite signal tracking capability |
Frequency |
BDS B1I/B2I/B3I , GPS L1/L2/L5 |
|
|
|||
GLONASS L1/L2 , GALILEO E1//E5a/E5b |
|||
Heading accuracy |
GNSS effective |
0.1° |
Dual antenna 2m baseline, single antenna requires dynamic alignment |
Maintaining accuracy |
0.15°/min |
GNSS failure |
|
Attitude accuracy |
GNSS effective |
0.1° |
RTK/ single point dual frequency |
Maintaining accuracy |
0.1° |
GNSS failure within 5 minutes |
|
Horizontal positioning accuracy |
GNSS effective |
1.2m |
Single point dual frequency |
1cm + 1ppm |
RTK |
||
Horizontal speed accuracy |
GNSS effective |
0.03m/s |
|
Timing accuracy |
GNSS effective |
20ns |
|
Gyroscope |
Measuring range |
±500 °/s |
|
Bias instability |
2 ° /h |
Allan variance |
|
Accelerometer |
Measuring range |
±8g |
|
Bias instability |
0.02mg |
Allan variance |
|
Data update rate |
GNSS data results |
10Hz |
Positioning / speed / heading / raw data information |
IMU Raw Data |
200Hz |
Default 100Hz |
|
Combined navigation solution results |
200Hz |
Default 100Hz |
|
Electrical Characteristics |
Communication interface |
LVTTL * 3 , CAN * 2 |
1 of 3 LVTTL direct- connect GNSS board |
Voltage |
3.3V DC |
|
|
Antenna power supply |
5V DC |
|
|
Power consumption |
≤ 1W |
|
|
Structural characteristics |
size |
40*30*5.15 mm |
|
weight |
≤ 20 g |
|
|
Usage Environment |
Operating temperature |
-40℃ ~ +85℃ |
|
Storage temperature |
-55℃ ~ +95℃ |
|
|
vibration |
6.06g ( 20~2000 Hz ) |
|
|
Shock |
40g / 11ms |
|
|
Note: All indicators without statistical method are RMS statistics. |