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MEMS Integrated Navigation System

ER-MINS-210/230(0.3~1.0°) Features
◆MEMS Inertial Navigation System
◆Provide horizontal attitude, Heading attitude, longitude, latitude, altitude
◆Used in unmanned aerial vehicles, vehicle navigation, aviation and platform stability control and other fields
  • ER-MINS-210/230


ER-MINS-210/230 MEMS Inertial Navigation System

ER-MINS-210/230 MEMS Inertial Navigation System , with high accuracy and high dynamic GPS receiver as the satellite signal sensor, use carrier phase differential technique and fast calculation of the whole week ambiguity technology. It can accurately calculate the azimuth angle of the carrier motion, inertial measurement technology aided attitude determination navigation. When the GPS signal interferences , by maintaining the inertial measurement unit within a period of time, system can still output high precision data


ER-MINS-210/230 MEMS Inertial Navigation Systemover comes the deficiency of a single device, give full play to the GPS high precision, with no accumulation error, no drift, low price and inertial products good dynamic performance, strong anti-interference ability. Without the need of external signal source, it is able to work and Improve the overall attitude measurement accuracy, navigation accuracy and real-time tracking performance of the system. The proof in the land, sea and air a variety of environmental test, heading accuracy of 0.1 degrees, roll and pitch accuracy 0.05 degrees, and effectively overcome the drift angle of heading error. 

It is multi system compatible and complement each other, mutual backup all-weather high reliability azimuth measurement products. Especially for satellite communication vehicle, meteorological radar vehicle, warship, expedition ship, airship, UAV, fire control system, command and control system, weapon aiming system, have very strong competitiveness.


ER-MINS-210/230 MEMS Inertial Navigation Systemcan provide horizontal attitude, heading attitude and other information, longitude, latitude, altitude, positioning information,the 3D acceleration, angular velocity inertial measurement information andetc. By extending the range of the mileage meter and the height of the barometer, it further improves the accuracy and applicability of the system and it can be widely used in unmanned aerial vehicles, vehicle navigation, aviation and platform stability control and other fields


Systematic Name



Performance Indicators


≤ 1.0 deg (1 σ)

≤ 0.3 deg (1 σ)

Horizontal Attitude

(Roll And Pitch)

≤ 0.5 deg (1 σ)

≤ 0.2 deg (1 σ)

Horizontal Position

2.5 m CEP

2.5 m CEP


4 m CEP

4 m CEP


≤ 0.2 m/s (1 σ)

≤ 0.1 m/s (1 σ)



±100 deg/s

±400 deg/s

Bias Stability

≤ 0.05 deg/s

≤ 10 deg/h

Bias Repeatability

≤ 0.05 deg/s

≤ 10 deg/h



±10 g(customizable)


Bias Stability

≤ 0.1 mg

≤ 0.1mg

Bias Repeatability

≤ 0.2 mg

≤ 0.2mg


GNSS Features

16 Channel,GPS
L1 Frequency Point

16 Channel GPSL1,

Positioning Time

≤ 60 s

≤ 60 s

Typical Recapture Time

≤ 10 s

≤ 10 s

Interface Features


9~36 Vdc

9~36 Vdc

Power Consumption

≤ 3.5 W @ 12 VDC

≤4W @24Vdc

Electrical Interface



Data Update Rate

100 Hz @ 115,200 bps

100 ~ 200Hz

Operating Environment

Operating Temperature

-40° C ~ +85° C

Storage Temperature

-55° C ~ +85° C


6 g @ 20~2000 Hz


30 g, 11 ms, 1/2 Sine

Physical Property

Physical Size

68.8×68×70 mm

86.8×68×87 mm


≤ 500 g

≤ 500 g


1. What is your quotation condition?

If you have DHL or Fedex account ,we can quote EXW price ,otherwise CIF or FOB price.


2.Do you have any discount when procurement? 

We will quote sample price at first and we will quote volume price if you need more quantity.


3.How long is the delivery time?

For sensors,parts,modules : in stock-one week;no stock-2-4weeks; For systems,generally ,8-12 weeks.


4.How to deal with the quality problems?

If confirmation of product quality problem we can replace it freely for customer in the shortest period.


If interested in MEMS Inertial Navigation System, pls contact us : ericco189@ericcointernational.com


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