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GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg

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GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg

Brand Name : FIREPOWER

Model Number : INS100E

Certification : CE

Place of Origin : China

MOQ : 1

Price : 2000$

Payment Terms : L/C,D/P,T/T,Western Union

Supply Ability : 1 week for sample

Delivery Time : 1 week

Packaging Details : Sponge + Carton

Heading accuracy : 0.1°

Attitude accuracy : 0.1°

Positioning accuracy : 1.5m;1cm+1ppm

Horizontal velocity accuracy : 0.1m/s

Gyroscope range : ±500°/s

Zero bias stability : 4°/h

Accelerometer range : ±16g

Acc Zero bias stability : 0.2mg

Dimension : 80mm × 53mm × 23mm

Interface : RS232/RS422

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Low Cost MEMS lnertial Navigation System with GPS for Land Vehicle

  • Product DescriptionGPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg

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.


  • System function

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.

  • Product Parameter

Project

Metrics (RMS)

Remark

Heading accuracy

GNSS valid ①

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

1.5m;1cm+1ppm

Single point L1/L2; Differential

Elevation, GNSS valid; RTK

2.5m;2cm+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

GPS-Enabled MEMS Inertial Navigation System for Land Vehicle ±16g Accelerometer Range and Acc Zero Bias Stability of 0.2mg



Product Tags:

Land Vehicle Inertial Navigation System

      

GPS-Enabled Inertial Navigation System

      

MEMS Inertial Navigation System

      
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