• Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System
  • Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System
  • Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System
  • Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System
  • Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System
  • Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System

Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System

Type: Piezoelectric
Output Signal Type: Digital Output
Measuring Shaft Quantities: 9
Accuracy Grade: 0.2G
IP Rating: IP67
Certification: ISO
Customization:
Gold Member Since 2024

Suppliers with verified business licenses

Jiangsu, China
  • Overview
  • Product Description
  • Product characteristics
Overview

Basic Info.

Model NO.
MLI3700
Customized
Customized
Data Transmission Interfaces
RS232/ RS422/RS485/Ttl/Can
Transport Package
Box and Sponge
Specification
14*15*5
Trademark
ML
Origin
China
HS Code
9031809090
Production Capacity
1000/Month

Product Description

Product Description

1.Combined Navigation Accuracy Index

Lost lock time Positioning mode Position accuracy Speed accuracy Pitch/roll accuracy Heading accuracy
3s Odometer access 1cm 0.03m/s 0.1° 0.2°
10s 1m 0.1m/s 0.1° 0.2°
60s 6m 0.1m/s 0.2° 0.35°
The sensor was in RTK positioning mode before losing lock.
2.Inertial sensor parameters
IMU Accelerometer Gyro Geomagnetic field Remark
Measuring range ±6g 500°/s ±8Gauss  
Resolution 0.001g  0.001°/s 0.25mg  
Bandwidth 150Hz   120Hz TBD 1
Bias stability 30uG 2.5°/h TBD  
Random walk 0.028m/s√h    0.3°/√h TBD  
Full temperature zero bias change <0.015°/s/ºC  <0.2mg/ºC  TBD 1
3.GNSS parameters
Index Describe Remark
Aisle 1408 channels  
Frequency BDS B1I/B2I/B3I GPS L1 C/A/L2P(Y)/L2C/L5
Galileo E1/E5a/E5b GLONASS L1/L2 QZSS L1/L2/L5
 
Cold start <30s  
Hot Start <2s  
RTK start time <5s  
Single point positioning accuracy RMS Level 1.5m Elevation 2.5m  
SBAS Level 0.4m Elevation 0.8m  
RTK positioning accuracy RMS Horizontal 0.8cm+1ppm Height 1.5cm+1ppm  
Orientation accuracy 0.2° /1m baseline  
update rate 20Hz  
Maximum speed 500m/s  
maximum height 50000m  
4.Mechanical and electrical parameter
Parameter Condition U310D
Input voltage 25ºC 6-36V DC
Power consumption 25ºC <1.8W
Size Aviation plug interface 75X60X25.2mm
Weight Aviation plug interface 180g
Shell material   Aluminum alloy
Operating temperature   -40-85ºC
Certification   CE, ROHS, IP68
5.Interface resources
Parameter Describe
COM1 Sensor data input and output interface, connected to the user host
COM2 Differential data input interface output GPGGA
RS-422 Sensor data input and output interface, connected to the user host
CAN1 Sensor data input and output, odometer data input
CAN2 reserve
PPS Timing signal PPS duty cycle 50%
SYNC Synchronous input and output pins
Hardware interface 12pin aviation plug
Data Update Maximum 100Hz(IMU), 100Hz(GNSS/INS)
Users can choose the appropriate hardware interface according to product requirements
6.Interface resources
Parameter Describe
Data output NMEA/RTCM/Novtel SPAN binary protocol
Data content Euler angles, quaternions, velocity, position, acceleration, angular velocity, etc.
Fusion algorithm EKF
External sensor support Odometer, GNSS, DTU, etc.
7.Interface electrical parameters
Parameter Condition Minimum value Typical value Maximum value Unit
Interface RS-232
Input voltage   -13.6   - 13.6 V
Input voltage threshold VIL   0.6 1.2 - V
Input voltage threshold VIH   - 1.5 2.4 V
Input resistance   3 5 7
Output impedance   300 - - Ω
Baud rate   9600/115200/230400/256000/460800/921600 Default 115200
Interface CAN2.0
Output voltage CAN H 2.75 3.5 4.5 V
Output voltage CAN L 0.5 1.5 2.25 V
Differential output voltage   1.5 - 3 V
Stealth output voltage   2 2.5 3 V
Maximum input voltage CAN H,CAN L -42 - 42 V
Baud rate   125K/250K/500K/1000K (default 500K)
Interface RS-422
Differential output voltage   2 - 3.2 V
Common mode output voltage   - - 3 V
Differential input threshold   -0.2 - 0.2 V
Input lag   - 25 - mV
Input resistance   12 15 -
SYNC IN
Input voltage   - - 3.6 V
ESD   -15 - 15 kV
SYNC OUT/PPS
Output voltage   - 3.3 - V
Output current   - 30 - mA
 
Product characteristics

 


I3700 is an integrated navigation system (GNSS/INS) composed of high-performance MEMS sensors, high-precision GNSS systems and high-performance microprocessors.  The built-in self-developed high-reliability integrated navigation algorithm can output the speed, position, attitude and other information of the measured carrier in real time. Users can also externally connect RTCM differential correction data to achieve high-precision RTK positioning. The IP68 waterproof shell-type package can be easily integrated into the user's system. Product model information is as follows:
Cost-Effective Digital Output Mins Micro Ins Mins325 Can Output Inertial Navigation System


 

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Gold Member Since 2024

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Trading Company
Registered Capital
2000000 RMB
Plant Area
501~1000 square meters