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AND-EX6-27-A MEMS Aerial Reference System

The product consists of MEMS inertial measurement unit, together with the heading attitude algorithm and complementary filtering algorithm with independent intellectual property rights. The system adopts MEMS device temperature error compensation technology and complementary filtering algorithm, which can maintain the attitude accuracy for a long time, adapt to the complex environment of high dynamics and high overload, and can output stable and reliable attitude information under dynamic environment.

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Product Details

Product Table

Parameters Unit Type
Heading angle drift (initial 0°, RMS) °/h 20
Pitch angle accuracy/roll angle accuracy (RMS) ° static:0.1
° dynamic:0.2
Gryos Measurement range °/s ±400
Zero-bias stability (10s smo 1σ, room Temp) °/h 3
zero bias full Temp.(10s smo 1σ, room Temp) °/h 20
Zero bias repeatability °/h 3
Random Walk °/√h 0.15
Cross coupling % 0.1
accelerometer Measurement range g ±10
Zero-bias stability (10s smo 1σ, room Temp) mg 0.05
zero bias full Temp.(10s smo 1σ, room Temp) mg 1
Zero bias repeatability mg 0.1
Cross coupling % 0.1
Data update rate Hz 500(customisable)
Voltage V 5±0.25
Power consumption W 1.5
Operating Temperature -45~80
Dimension mm 54*54*25
Weight g 80
Interface RS-422

FAQ

What are the quotation methods?

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

Are there any discounts?

After we submit the sample price, if more quantity is needed, we will quote the bulk price.

How long will it take to deliver the goods after placing the order?

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

How to deal with quality problems?

After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.

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