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SNC100C-LITE MEMS Integrated Navigation System
  • SNC100C-LITE MEMS Integrated Navigation System

SNC100C-LITE MEMS Integrated Navigation System

Place of Origin China
Product Details
Payment & Shipping Terms
Minimum Order Quantity
1 Set
Packaging Details
Carton
Delivery Time
Peak Season Lead Time: one month Off Season Lead Time: one month
Payment Terms
LC, T/T, D/P, PayPal, Western Union
Product Description
Description
About The SNC100C-LITE MEMS Integrated Navigation System
Product overview
SNC100C-LITE integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation solution algorithm, and has short-term inertial navigation ability when GNSS is invalid. The product has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in tactics and industry, no system, and intelligent ammunition.

1. Product features
Built in high-precision ten axis IMU
The accuracy is guaranteed within the full temperature range (- 40 ℃ ~ 70 ℃)
Small size and light weight
With shaking / moving base alignment function

2. Main application fields
Tactical and industrial UAV
Intelligent ammunition
Dynamic communication
Unmanned ship, unmanned vehicle
Automatic driving

3 Working principle
The inertial measurement unit is composed of three accelerometers and three gyroscopes. It is responsible for measuring the acceleration and angular velocity of the carrier and sending these information to the information processing circuit. The information processing circuit uses the acceleration and angular velocity measured by the inertial measurement unit for navigation settlement, and takes the satellite navigation information received by the GNSS receiver as the reference for integrated navigation, The navigation error of inertial navigation is corrected, and the navigation information is output through the information interface circuit.

4. Performance index
Project Indicator(RMS)
Heading accuracy Dual GNSS 0.1°
Single GNSS 0.2°
Post processing 0.03°
Maintain accuracy 0.2°/min
Attitude accuracy GNSS valid 0.1°
Inertia / odometer combination 0.1°(RMS)
Post processing 0.02°
Maintain accuracy 0.2°/min
V-G mode
Horizontal positioning accuracy GNSS valid 1.2m
2cm+1ppm
Inertia / odometer combination 2‰D(D represents mileage,CEP)
Post processing 1cm+1ppm
GNSS failure 20m
Horizontal velocity accuracy GNSS valid 0.1m/s
Inertia / odometer combination 0.1m/s(RMS)
Inertial / DVL combination 0.2m/s(RMS)
Gyroscope Measuring range ±450°/s
Zero bias stability 2°/h
Accelerometer Measuring range ±16g
Zero bias stability 30µg
communication interface RS232 1way
RS422 1way
CAN 1way
Odometer differential input 1way
PPS output 1way
EVENT input 1way
Electrical characteristics Voltage 5~36VDC
power waste ≤3W
Ripple 100 mV
Structural characteristics Size 80 mm×53 mm×23mm
Weight ≤150g
Use environment Working temperature -40℃~+60℃
Storage temperature -45℃~+65℃
Vibration 20~2000Hz,6.06g
To attack 30g,11ms
Degree of protection IP65
Reliability MTBF 30000h
life >15年
Continuous working time >24h


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