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Inertial Navigation System
Created with Pixso.

High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer

High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer

Brand Name: Firepower
Model Number: INS100C-C0
MOQ: 1
Price: negotiable
Payment Terms: L/C, T/T
Detail Information
Place of Origin:
CHINA
Certification:
CE
Gyro Range:
±450°/s
Gyro Bias Stability:
≤0.5°/h
Accelerometer Range:
±16g
Accelerometer Bias:
≤100ug
Heading Accuracy:
0.1 °/L (RMS)
Attitude Accuracy:
0.05°(RMS)
Horizontal Velocity Accuracy:
0.05m/s
Interface:
RS232/RS422
Weight:
≤200g
Size:
80*60*38mm
Packaging Details:
Sponge/Box
Highlight:

High Accuracy Inertial Navigation System

,

MEMS Gyroscope Inertial Navigation System

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Accelerometer Inertial Navigation System

Product Description

High Accuracy Integrated Inertial Navigation System with Built-in MEMS gyroscope and accelerometer

 

Product Description

 

INS100C-C0 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 algorithm, and have short-term inertial navigation capability when GNSS is invalid.

 

The product has high reliability and strong environmental adaptability. By matching different software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.
 
Main Function
 
The integrated navigation system can use the satellite navigation information received internally to carry out integrated navigation, and output the information of the carrier, such as pitch, roll, heading, position, speed, time and the like; After losing the satellite signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time.
 
Technical parameters
 
Project
Metrics (RMS)
Remark
 
Heading accuracy

 

Dual GNSS
0.1°
2m baseline
Single GNSS
0.1°
 
Maintain accuracy
≤0.3°
GNSS failure 0.5h
 
Attitude accuracy

 

GNSS is valid
0.05°
 
Maintain accuracy
≤0.3°
GNSS failure 0.5h
 
 
Horizontal positioning accuracy
 
GNSS is valid
1.2m
Single point L1/L2
2cm+1ppm
RTK
Maintain accuracy
≤1nm
GNSS failure 10min
 
 
Horizontal velocity accuracy

 

 
GNSS is valid

 

 
0.05m/s
 
 
Gyroscope

 

Measuring range
±450°/s
 
Zero bias stability
≤0.5°/h
10 s average
 
Accelerometer
Measuring range
±16g
 
Zero bias stability
≤100µg
10 s average
 
 
Communication interface
 
RS232
 
Route 1
Optional CAN,
odometer
RS422
Route 1
 
 
 
Electrical characteristics
Voltage
9~36VDC
 
Power consumption
≤6W
 
Ripple
100 mV
P-P
 
Structural characteristics
Size
80 mm×60mm×38mm
 
Weight
≤200g
 
 
 
Use environment
Operating temperature
-40℃~+60℃
 
Storage temperature
-45℃~+70℃
 
Vibration
20~2000Hz,6.06g
 
Impact
30g,11ms
 
 
Reliability
MTBF
30000h
 
Continuous working time
>24h
 
 
Outline Drawing
 
High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer 0
Detail Photo
 
High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer 1
High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer 2

Payment & Shipping

 

 

High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer 3

High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer 4

High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer 5