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Inertial Navigation System
Created with Pixso.

Low Cost Mems Integrated Navigation System with RS232/RS422 Output

Low Cost Mems Integrated Navigation System with RS232/RS422 Output

Brand Name: FIREPOWER
Model Number: INS500D
MOQ: 1
Price: 7000$
Payment Terms: L/C,T/T,Western Union
Supply Ability: 500/month
Detail Information
Place of Origin:
China
Heading Accuracy:
0.1°
Attitude Accuracy:
0.1°
Gyro Range:
±500°/s
Gyro Zero Bias Stability:
4°/h
Acc Range:
±16g
Acc Zero Bias Stability:
0.2mg
Vibration:
20~2000Hz
Weight:
≤150g
Communication Interface:
PPS, Event, RS232, RS422, CAN
Horizontal Velocity Accuracy:
0.1m/s
Packaging Details:
sponge+box
Supply Ability:
500/month
Highlight:

RS422 Mems Integrated Navigation System

,

Low Cost Mems Integrated Navigation System

,

RS232 Mems Integrated Navigation System

Product Description

Product Description


INS100E integrated navigation system (hereinafter referred to as 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 have short-term inertial navigation capability when GNSS is invalid.

The product has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in the fields of industry unmanned motion carrier, unmanned vehicle, unmanned ship, communication in motion, mapping, stable platform and so on.


The integrated navigation system can carry out integrated navigation by using the satellite navigation information received internally, and output the pitch, roll, heading, position, speed, time and other information of the carrier; 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

GNSS valid

0.1°

 

Heading holding

0.2°/min

GNSS failure

Attitude accuracy

GNSS is valid

0.1°

Single-point L1/L2, RTK

Attitude holding

0.2°/min

GNSS failure

Positioning accuracy

Horizontal, GNSS valid; RTK

1.5m1cm+1ppm

Single point L1/L2; Differential

Elevation, GNSS valid; RTK

2.5m2cm+1ppm

Single point L1/L2; Differential

Position holding, GNSS failure

20m

Unlocked for 60s

Horizontal velocity accuracy

GNSS is valid

0.1m/s

Single-point L1/L2,RTK

Gyroscope

Measuring range

±500°/s

 

Zero bias stability

4°/h

Allan variance

Accelerometer

Measuring range

±16g

Customizable 200 g

Zero bias stability

0.2mg

Allan variance

Satellite board

Cold start

< 30 seconds

Open environment

Hot start

5 seconds

Open environment

Type of receiver

BDS B1I/B2I/B3I

GPS L1C/A/L2P (Y)/L2C/L5

GLONASS G1/G2

Galileo E1/E5a/E5b

QZSS L1/L2/L5

 

Communication interface

RS232

Route 2

 

RS422

Route 1

 

Electrical characteristics

Voltage

9~36VDC

 

Power consumption

≤3W

 

Ripple

100 mV

P-P

Structural characteristics

Size

80 mm×53 mm×23mm

 

Weight

≤150g

 

Use environment

Operating temperature

-40℃~+60℃

 

Storage temperature

-45℃~+65℃

 

Vibration

20~2000Hz,6.06g

 

Impact

30g,11ms

 

Degree of protection

IP65

 

Reliability

MTBF

30000h

 

Life span

> 15 years

 

Continuous working time

>24h

 

 Effective 2m baseline of dual antenna, or dynamic alignment of single antenna


 Outline Drawing

Low Cost Mems Integrated Navigation System with RS232/RS422 Output 0