High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics

Product Details
Customization: Available
Data Transmission Interfaces: RS232/ RS422/RS485/Ttl/Can
Transport Package: Box and Sponge
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  • High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
  • High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
  • High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
  • High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
  • High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
  • High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
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Basic Info.

Model NO.
U3700
Specification
14*15*5
Trademark
ML
Origin
China
HS Code
9031809090
Production Capacity
1000/Month

Product Description

Parameter U3700-A U3700-B U3700-C U3700-D Unit
Attitude Precision
Pitch (±90°) /Roll (±18) (static) 0.15(normal), 0.2(max) °
Pitch (±90°) /Roll (±18) (dynamic) 0.15(normal) 0.3(max) 0.15(normal)
0.2(max)
°
Yaw (±18) static drift 2hrs (6DOF) (1) 0.15(normal), 0.2(max) °
 
Yaw (±18) dynamic drift (6DOF) (2) 9
 
5 5 5 °
Magnetic assist (AHRS)(3) 2(normal), 3(max) °
Yaw rotation error (6DOF) (rotation under 100°/s)(4) 3(max) <0.8(normal) 1.3(max) <0.8(normal) 1.3(max) 1(max) °
Resolution 0.01 °
Note:
(1)  Module horizontally stationary for 2 hours.
(2)  The module was measured after 1 hour of movement on an indoor robot, 1σ
(3)  After geomagnetic calibration, the product needs to be configured in AHRS mode when there is no magnetic field interference in the surrounding area.
(4)  The turntable rotates continuously for 10 turns, and the heading angle accumulates error.
3-Axis Gyroscope U3700-A U3700-B U3700-C U3700-D Unit
Measurement range ±2000 (adjustable) °/s
Resolution 16 bit
Scale factor(100°/s)(1)  <600(normal)
800(max)
<280(normal)
350(max)
<280(normal)
350(max)
<280(normal)
300(max)
ppm
Nonlinearity(2) ±0.05 %Fs
3dB Bandwidth 47(normal) - 230(max) Hz
Sampling 1000 Hz
Zero bias instability (Allan)(3) 5.1 2.5 2.5 1.76 °/h
Zero bias repeatability (Allan)(3) 0.09 0.05 0.05 0.03 °/s
Angle random walk (Allan)(3) 0.6 0.3 0.3 0.21 °/√h
Full temperature zero bias-40-85ºC(4) Z: 0.015(normal) - 0.035(max)
Y: 0.05(normal) - 0.018(max)
X: 0.03(normal) - 0.08(max)
°/s
Accelerometer sensitivity (All three axis) 0.1 °/s/g
Notes:
(1) : Rotate the turntable 10 times in both directions and take the average measurement
(2) : Maximum deviation from the best fit line within the specified range
(3) : Refer to the 5.1 ~ 5.3 -Alan variance curve
(4) : The temperature rise slope measured by the temperature chamber turntable in the lab is less than 3ºC/min. For detailed data, please refer to Figure 13 for the temperature compensation curve
 
3-Axis Accelerometer U3700-A U3700-B U3700-C U3700-D Unit
Measurement range ±12(adjustable) g
Resolution 16 bit
Initial bias drift(1) 5(max) mg
Nonlinearity 0.5(normal) %Fs
3dB Bandwidth 145 Hz
Sampling 1600 Hz
Zero bias instability (Allan)(2) 0.06 0.03 0.03 0.021 mg
Zero bias repeatability (Allan)(2) 2.52 1.5 1.5 0.6 mg
Angle random walk (Allan)(2) 0.08 0.04 0.04 0.028 m/s/√h
Full temperature zero bias-40-85ºC(3) 1(normal) - 2.5(max) mg
Notes 
(1) : After user installation, this value may change according to actual conditions, refer to 7.8 for initial zero bias
(2) : Refer to the 5.1~5.3 Alan variance curve
(3) : The temperature rise slope measured by the temperature chamber turntable in the lab is less than 3 ºC/min. For detailed data, please refer to Figure 13 for the temperature compensation curve
Magnetometer U3700-A U3700-B U3700-C U3700-D Unit
Range ±8 Gauss
Resolution (Fs=2G) 2 mGuass
Sampling 200 (normal) Hz
Linearity (Best fitting straight line Fs=2G) 0.1 (normal) Fs%
Temperature sensor U3700-A U3700-B U3700-C U3700-D Unit
Range -104(min) - 150(max) ºC
Offset error ±1 K
Mechanical/Environment U3700-A U3700-B U3700-C U3700-D Unit
Power supply 7 - 48 V
Power consumption 300 400 400 600 mW
Working temperature -40 - +85 ºC
Gyroscope range ±125(min) -±2000(normal/max) °/s
Accelerometer range ±3(min) -±12(normal) -±24(max) g
Starting time(1) 2 s
Size M12 connector interface: 58.5*40*20
PG connector interface: 40*36*16
mm
Weight <75 g
Shell material and process Aluminum alloy CNC  
Assembling screws M3  
Anti-Vibration 1.0mm(10Hz-58Hz) &≤20g(58Hz-600Hz)  
Shock (duration <1ms) 2000 g
Environment protection RoHS Directive 2011/65/EU  
EMC LVD Directive 2014/35/EU  
Drop test Free fall 3 times on a 75cm high experimental platform  
Temperature shock Raise the temperature from -40 to 85 ºC within 1h, 5 times  
Notes:
(1)  Startup time refers to the time it takes for the system to shut down and output valid data. During this period, the module should be kept stationary
Interface Min Normal Max Unit
UART Baud-rate(1) 9600 115200 921600 bps
Starting position 0 1   bit
Data length 0 8   bits
Stop bit   1   bit
Checksum   None   bit
Output framerate(2) 0 100 1000 Hz
Input impedance
Output impedance
(Rs232)
3
300
5
10M
7
Ω
CAN Baud-rate(3) 125 500 1000 kbps
Output framerate(4) 5 100 200 Hz
Input impedance(5) (with 120 Ω resistor)
(without 120 Ω resistor)



19

120

30



52

Ω


 
RS485 Baud-rate (Modbus)
(non-Modbus)

9600
9600

115200
115200

115200
921600

bps
Starting position 0 1   bit
Data length 0 8   bits
Stop bit   1   bit
Checksum   None   bit
Output framerate
(Modbus)
(non-Modbus)

0
0

10
100

50
250

Hz
Input impedance(5) (with 120 Ω resistor)
(without 120 Ω resistor)



48

120

 

Ω


 
Trigger
Pin
Logic voltage High
           Low
2.0  
0.6
V
Delay (From triggering to data transmission)(6)     800 us
Notes:
(1) If modifications are required, please refer to the instruction and programming manual.  
(2)  The sensor supports data output at 1, 5, 10, 50, 200, 250, 500, and 1000 Hz.  
(3)  If modifications are required, please refer to the instruction and programming manual.  
(4)  The sensor supports 5, 10, 50, 100, and 200 Hz data output.  
(5)  By default, there is no 120 Ω resistor connected
(6)  Please refer to the synchronization function chapter and instruction and programming manual for triggering timing and configuration.
Environment
Working temperature -40 ~ +80 ºC
Storage temperature -40 ~ +95 ºC
Anti-Vibration 1.0mm(10Hz-58Hz) &≤20g(58Hz-600Hz)  
Shock (duration <1ms) 2000 g
High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/RoboticsHigh Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/RoboticsHigh Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics
High Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/RoboticsHigh Performance Mems Imu U3700 Series - 6dof Ahrs/Vru with Kalman Filter, RS485/Can/Uart, for Uav/Robotics 
COMPANY INFORMATION
ML is a national high-tech enterprise that has been focusingon using inertial navigationand information fusion technology to solve the accuracy and real-time needs ofvarious types ofmoving objects for navigation information such as position and attitude. Our products coverhigh-tech sensor products from MEMS industrial-grade inertial navigation chips to high-precisioninertial navigation modules, which are mainly used in autopilots ofunmanned systems (includingautopilot/drones/unmanned ships) , satellite tracking,robots, intelligent pursuit, high-speedrail/bridge/dam mapping and other fields.
ML has accumulated strong product R&D and innovation capabilities through years ofaccumulation in chip design, process manufacturing, industry algorithms and calibration capabilitiesin the MEMS inertial industry. At present, the company has obtained several invention patents andsoftware copyrights, covering MEMS inertial navigation chips and modules, and has successfully usedthese patents to realize product transformation.


 

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