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Asset ID: quartz-mems-nav-dgys60cj10
DGYS60CJ10
Navigation / Quartz Mems / Nav Modules

DGYS60CJ10

High-reliability MEMS inertial navigation system, integrates 3-axis quartz MEMS gyroscope, 3-axis MEMS accelerometer, signal processing and navigation software, suitable for aerospace, mechanical control, exploration, marine, and port applications.

Power Supply Voltage

5 ± 0.2 V

Operating Current

≤150 mA

Weight

90 ± 5 g

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The DGYS60CJ10 is a high-reliability MEMS inertial navigation system composed of a three-axis quartz MEMS gyroscope, a three-axis MEMS accelerometer, signal processing circuitry, and integrated navigation software. It supports navigation, ranging, and attitude estimation functions, and is suitable for aerospace, mechanical control, exploration, marine, and port applications.

Key Features

  • 3-axis quartz MEMS gyroscope + 3-axis MEMS accelerometer
  • Integrated signal processing and navigation software
  • Supports navigation, ranging, and attitude estimation
  • High reliability, suitable for aerospace and industrial applications

Applications

AerospaceMechanical controlExplorationMarinePort applications

Technical Specifications

Key Technical Specifications

Power Supply Voltage

5 ± 0.2

V

Operating Current

≤150

mA

Weight

90 ± 5

g

Startup Time

≤2

s

Gyroscope Specifications

Measurement Range

ñ300

°/s

Scale Factor

1 ± 0.005

Scale Factor Nonlinearity

≤100

ppm

Scale Factor Repeatability

≤100

ppm

Scale Factor Asymmetry

≤100

ppm

Cross-Axis Sensitivity

≤0.005

Threshold / Resolution

≤0.01

°/s

Bias (Full Temperature)

±0.05

°/s

Bias Stability (Room Temp)

≤10

°/h

Bias Stability (Full Temp)

≤50

°/h

Bias Repeatability

≤10

°/h

Angular Random Walk

≤0.12

°/√h

Bias Instability (Allan Deviation)

≤2

°/h

Bandwidth (Amplitude)

√120

Hz

Delay Time

√2.0

ms

Accelerometer Specifications

Measurement Range

√10

g

Bias (Full Temperature)

±5

mg

Bias Stability (Room Temp)

≤0.2

mg

Bias Stability (Full Temp)

≤2

mg

Bias Repeatability

≤0.2

mg

System Positioning Performance (Dual-Antenna GPS, 1m Baseline)

Heading Accuracy

≤0.2

°

Attitude Accuracy

≤0.1

°

Velocity Accuracy

≤0.1

m/s

Horizontal Position Accuracy

≤3

m

Vertical Position Accuracy

≤5

m

GPS Outage Hold Performance (@60s)

Heading Accuracy

≤0.5

°

Attitude Accuracy

≤0.3

°

Horizontal Position Accuracy

≤45

m

Vertical Position Accuracy

≤15

m

System Measurement Ranges

Heading Measurement Range

0 ~ 360 (CW from North)

°

Attitude Measurement Range

Roll: -180 ~ +180

°

Pitch Measurement Range

Pitch: -85 ~ +85

°

Environmental Adaptability

Vibration (6.06g RMS, 20Hz–2kHz)

≤36

°/h / mg

Shock (Half-Sine, 200g, 6ms)

≤36

°/h / mg

Operating Temperature

-45 ~ +85

℃

Storage Temperature

-55 ~ +85

℃

Technical Documentation

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Datasheet (PDF)

Full performance curves, pinout diagrams, and environmental testing results.

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CAD Model (STEP)

High-fidelity 3D geometry for structural integration and thermal modeling.

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Compliance Documentation

Certification of origin, quality management protocols, and compliance documentation.

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All specifications can be customized. Tell us your requirements for a tailored solution.