High Accuracy North-Seeking MEMS IMU
Inertial Measurement Unit, referred to as IMU, is a device to measure the attitude angle (or angular velocity) and acceleration of the three axis of the object. Gyroscope and accelerometer are the core devices of inertial navigation system (INS). With the built-in accelerometer sensor and gyroscope, the IMU can measure the linear acceleration and rotation angular velocity from three directions and can obtain the attitude, velocity and displacement information of the carrier through the resolving.
ER-MIMU-01 uses MEMS accelerometer and gyroscope with high quality and reliability, RS422 and external communication, baud rate can be flexibly set between 9600~921600, through the communication protocol to set the user’s required communication baud rate. With X, Y, Z three-axis precision gyro, X, Y, Z three-axis accelerometer with high resolution, can be output by RS422 X, Y, Z three axis of gyroscope and accelerometer’s original hexadecimal complement data (including gyro hexadecimal complement the numerical temperature, angle, the accelerometer hexadecimal temperature, the acceleration hexadecimal complement number); It can also output float dimensionless values of the gyroscope and accelerometer processed by the underlying calculation.
Bridge, tall building, tower, dam monitoring
Navigation and control
Attitude reference system
Vehicle and ship attitude measurement
Integrated inertial/satellite navigation system
Drilling and production systems
Mobile mapping system
Volume: 44.84 mm×38.88 mm×21.39 mm;
5V power supply, low power consumption 1.0W;
Light weight: ≤60g;
Products include X, Y, Z three-axis MEMS gyro and X, Y, Z three-axis MEMS accelerometer;
RS422 bus communication, baud rate from 9600~921600 can be set.
|Scale Factor at 25°C||80000||lsb/deg/s|
|Scale Factor Repeatability (1σ)||<50||ppm|
|Scale Factor VS Temperature (1σ)||300||ppm|
|Scale Factor Non-Linearity (1σ)||<200||ppm|
|Bias stability (10s 1σ)||<0.1||°/hr|
|Angular Random Walk||<0.005||°/ √h|
|Bias error over temperature (1σ)||3||°/Hr|
|Bias temperature variations, calibrated (1σ)||<0.3||°/Hr|
|Bias Repeatability (1σ)||<0.1||°/hr|
|Bias Stability (1s) (1σ)||<20||<30||μg|
|Bias Temp Coefficient||<10||<20||μg/℃|
|Bias Temp Hysteresis||<0.5||<0.5||mg|
|Factor Scale Non-linearity||<500||<500||ppm|
|Factor Scale Repeatability||<300||<300||ppm|
|Factor Scale Temp Coefficient||10||10||ppm/℃|
|Class II Non-linearity Coefficient||<100||<100||μg/g²|
|Operate Temp||-45℃~+ 85℃|
|Storage Temp||-55℃~+ 105℃|
|Size||44.84 mm×38.88 mm×21.39 mm|
1. What are the quotation methods?
If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.
2. Are there any discounts?
After we submit the sample price, if more quantity is needed, we will quote the bulk price.
3. How long will it take to deliver the goods after placing the order?
For sensors, parts and modules: in stock-one week; no stock-2-4 weeks; For systems, generally, 8-12 weeks.
4. How to deal with the quality problems?
After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.
If interested in High Accuracy North-Seeking MEMS IMU, pls contact us: email@example.com