ER-FIMU-50 Minimum FOG IMU
Introduction
ER-FIMU-50 FOG IMU is a minimum cost-effective inertial measurement device for navigation, control and dynamic measurement. The system adopts high reliability closed-loop fiber optic gyroscope and accelerometer, and ensures the measurement accuracy through multiple compensation techniques. Strict technology is adopted in the manufacturing process to ensure that the angular motion and linear motion parameters of the carrier can be accurately measured under harsh conditions.
The product has a great user experience. In addition to the wide-voltage power supply, users can also configure the output bandwidth, data update rate, communication port baud rate and communication protocol according to their needs.
Features
Minimum optical fiber IMU
Full temperature compensation
Strong shock resistance and vibration resistance
Bandwidth>100Hz
Data update rate: 100Hz~4000Hz
Baud rate configurable, up to 921.6Kbps
Weight<600g
Wide voltage supply 9V~31V
Power consumption 4.8 W
Applications
AHRS
Guidance control system
Vehicle and ship attitude measurement
Inertial/satellite integrated navigation system
Drilling system
Mobile mapping system
Satellite communication in motion
Specifications
FOG Gyro | |
Measuring range | 500°/s |
Bias stability | 0.5°/h |
Bias repeatability | 0.5°/h |
Scale factor non-linearity | 100ppm |
Bandwidth | 50Hz~200Hz |
Angular random walk | 0.02°/sqrt (h) |
Accelerometer | |
Measuring range | ±25g |
Bias stability | 100ug |
Bias repeatability | 100ug |
Scale factor non-linearity | 300ppm |
Electrical/Mechanical Interface | |
Power supply | 9V~31V |
Power | <4.8W |
Starting time | 3s |
Interface | RS-422 |
Update Rate | 100Hz~4000Hz |
Size | F89mm*73mm |
Weight | <600g |
Operating environment | |
Working temperature | -40°C~60°C |
Storage temperature | -55°C~70°C |
Vibration | 6.06g (rms) |
Impact | 80g/3ms |
Interface Definition
External use of J30J-15TL connector for communication
No. | Definition |
1 | RS422_Tx+ |
2 | RS422_Tx- |
3 | RS422_Rx- |
4 | RS422_Rx+ |
5 | / |
6 | CFG_Rst- |
7 | Msync- |
8 | TOV_OUT- |
9 | GND |
10 | VDD |
11 | Msync- |
12 | TOV_OUT+ |
13 | CFG_Rst- |
14 | DGND |
15 | / |
Communication Protocol
FOG IMU default timing broadcast mode output IMU data, output frequency 4K, 19 bytes of data per frame, baud rate 921600bps, 1 bit start, 8 bit data, 1 bit stop, no check, multi-byte variables, high bytes first, low bytes later. Communication protocols can also be customized to the user's requirements.
No. | Name | Equivalent | Unit | Data Type | Remark |
1 | 0xCC | / | / | Unsigned integer | fixed frame head |
2 | Send a count | 1 | / | Unsigned integer | 0-200, 255 breakdown |
3-5 | X Gyro | 0.00006 | D/Sec. | Integer | Angular rate |
6-8 | Y Gyro | 0.00006 | D/Sec | Integer | Angular rate |
9-11 | Z Gyro | 0.00006 | D/Sec | Integer | Angular rate |
12-13 | X Accelerometer | 0.008 | M/Sec2 | Integer | Accelerated speed |
14-15 | Y Accelerometer | 0.008 | M/Sec2 | Integer | Accelerated speed |
16-17 | Z Accelerometer | 0.008 | M/Sec2 | Integer | Accelerated speed |
18 | Temperature | 1 | degree centigrade | Integer | / |
19 | Checksum | 1 | / | Unsigned integer | 2-18 bytes |
Dimension
Application Techniques
1.Internal Structure Analysis of IMU
2.What are the Application Scenarios of the IMU?
3.Application of IMU in UAV Flight Control System
4.IMU in Drones (MEMS triaxial accelerometer, triaxial gyroscope, triaxial magnetometer)
6.IMU inertial measurement unit (provides odometer, position, attitude)