MNS300E Attitude Determination Instrument

Introduction

  • Accurate parameter calibration
  • Built-in shock absorption module
  • Full temperature compensation.

The MNS300E consists of a MEMS three-axis gyroscope and a three-axis accelerometer. It can meet the performance requirements under different conditions after full temperature calibration. The product provides stable and reliable attitude information, angular rate and linear acceleration information for the carrier through a built-in unique attitude algorithm. The product has the advantages of small size, low power consumption, high reliability and stable performance and can be used in attitude control of vehicle, airborne, shipborne and other fields.

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Description

Performance

Gyroscope

Accelerometer

Range ±450 ° /s Range ±10 g
Bias Stability ≤10 ° /h Bias ≤5 mg
Bias Repeatability ≤10 ° /h Bias Stability ≤0.2 mg
Scale Factor Nonlinearity ≤50 ppm Bias Repeatability ≤0.2 mg
Angular Random Walk ≤0.2 ° /√h Scale Factor Nonlinearity (within ± 1g) ≤150 ppm

Roll/pitch

Static ≤0.1 °
Dynamic ≤0.3 °
Heading
Heading drift@1min ≤0.2 °

 

System

Supply Voltage 5 ±0.2 V
Power ≤2 W
Digital Interface RS422
Update rate 200(Up to 500) Hz
Baud rate 115200 default bps
Working Temperature -45~+85 ° C
Storage temperature range -50~+85 ° C
Weight ≤75 g
Connection J30J-15ZKP connector

 

Application

  • Space-based fields: missile loading, load stabilization, drones
  • Land-based fields: precision agriculture, mobile communication
  • Sea-based fields: underwater unmanned platforms, ship positioning, communication unmanned ships

 

Dimension and wiring definition

Dimension Output
MNS300E Dimension 300x144 - MNS300E Attitude Determination Instrument No. Definition Description
1 +5V Power+
2 GND Power ground
3 RS422_TX_P RS422 transmit +
4 RS422_TX_N RS422 transmit –
5 RS422_RX_P RS422 receive +
6 RS422_RX_N RS422 receive –
7 AUX_RS232_TXA Extended serial port output
8 AUX_RS232_RXA Extended serial port input
9 SGND Signal ground
10 N/A N/A