陕西艾瑞科 ER-MG2-300/400 mems gyroscope

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  • ER-MG2-300/400

  • mems gyroscope

  • 陕西艾瑞科

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  • Ericco 艾瑞科

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Introduction

ER-MG2-300/400, a Navigation Grade MEMS gyro sensor up to 400deg/s measurement range and 0.05°/hr bias instability, is specially designed for precision attitude & azimuth measuring, positioning, navigating, guidance in high performance IMU /AHRS/ GNSS-aided INS, aerial/marine/land mapping/survey system/UAV/AUV and navigation grade MEMS weapon system.With the high dynamic measurement range and high precision, ER-MG2-300/400 is a cost effective, robust, reliable, small size, light weight, low power, most suitable replacement of medium-low navigation grade FOG/DTG with high dynamic azimuth & attitude measuring , inertial positioning and navigation function in aerial, marine manned, or unmanned carriers.

The ER-MG2-300/400 High Precision Navigation MEMS Gyroscope is a single-axis MEMS angular rate sensor (gyroscope), capable of measuring angular velocity up to a maximum of ±400°/s with digital output compliant to SPI slave mode 3 protocol. Angular rate data is presented as a 24-bit word.

The ER-MG2-300/400 with an advanced, differential sensor design rejects the influence of linear acceleration, enables to operate in exceedingly harsh environments where shock and vibration are present.The ER-MG2-300/400 is available in a hermetically sealed ceramic LCC surface mount package, and is capable of operating at 5V supply and a wide temperature range (−40°C to +85°C).


Features

Proven and robust silicon MEMS gyro

Up to ±400°/s measurement range

0.03-0.05°/hr bias instability

0.01-0.025°/√hr angular random walk

Digital output (SPI slave)

5V operation (4.75~5.25V supply)

Low power consumption (40 mA)

High shock and vibration rejection

Hermetically sealed ceramic LCC surface mount package (11x11x2mm)

Integrated temperature sensorRoHS compliant


Application areas

Precision attitude & azimuth keeping, positioning, navigation in navigation grade IMU/INS/AHRS

Heading, navigation, positioning in High performance GNSS-aided INS

Orientation, navigation, positioning in aerial/marine/land mapping/survey system

Attitude and motion control in medium and large UAV, AUV

Pointing and tracking in satellite antenna,target tracking system

Guidance and navigation in medium-low navigation grade MEMS weapon system

Azimuth, position, heaving/swaying/surging of gyrocompass in surface and submarine carriers, AUV

Antenna and Line of Sight Stabilization Systems

Integrated Navigation Systems & Inertial Guidance System

Flight Control & Guidance System

Attitude Heading Reference Systems (AHRS)

Stabilization of Antennas, Cameras & Platforms

Aerial and Marine Geo-mapping / Surveying


Specifications

ParameterER-MG2-300ER-MG2-400Unit
Range300400deg/s
Resolution2424bits
Data Rate12K12KHz
Group delay<5<3ms
Bandwidth (-3dB)50100Hz
Scale Factor at 25°C2800020000lsb/deg/s
Scale Factor Repeatability (1σ )<50<20ppm
Scale Factor VS Temperature (1σ )300100ppm
Scale Factor Non-Linearity (1σ)<300100ppm
Bias Instability0.030.05deg/hr
Bias stability (1σ 10s)0.15<0.5deg/hr
Bias stability (1σ 1s)0.5<1.5deg/hr
Angular Random Walk<0.01<0.025°/ √h
Bias error over temperature (1σ)103deg/hr
Bias temperature variations, calibrated (1σ)<1<0.5deg/hr
Bias repeatability (1σ )<0.3<0.3deg/hr
Noise Peak to Peak±0.01±0.05deg/s
G-Sensitivity<1<1°/hr/g
Vibration rectification error<1<1°/hr/g (rms)
Startup Time11s
Sensor Resonant Frequency11K~13K
Environment, Power and Physical
Shock (charged)1000g,1ms, half sine wave
Shock (uncharged)10000g,1.0ms, half sine wave
Vibration (Operating)12grms, 20Hz to 2KHz random vibration
Operating Temperature-40°C~85°C
Max storage (survival) Temperature-55°C~125°C
Supply voltage5±0.25V
Current consumption40mA


ER-MG2-300/400 mems gyroscope技术参数

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性 能
随机游走 0.01-0.025 deg/hr/sqrt
零偏稳定性 0.15-0.5 deg/hr
特 性
角速率量程 300-400 deg/sec
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