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HDTD80CJ12
Navigation / Quartz Mems / Nav Modules

MEMS Inertial/GNSS Integrated Navigation System (Single-Antenna)

MEMS Inertial/GNSS Integrated Navigation System · HDTD80CJ12

Single-antenna MEMS inertial/GNSS integrated navigation system combining quartz MEMS gyroscopes (±300–±400 °/s), MEMS accelerometers (±10–±40 g), and a high-precision GNSS module for differential positioning and orientation. Heading accuracy ≤0.3 ° at speeds of 5 m/s and above, attitude accuracy ≤0.1 °, −45 °C to +85 °C.

Power Supply Voltage

5 ± 0.2 V

Operating Current @12V

135 ± 10 mA

Weight

75 ± 5 g

Product Gallery

The HDTD80CJ11 is a high-reliability MEMS inertial/GNSS integrated navigation system. It integrates a three-axis quartz MEMS gyroscope, a three-axis MEMS accelerometer, a high-precision single-antenna GNSS positioning module, signal processing circuits, and integrated navigation software. This configuration enables high-precision differential positioning, orientation, navigation, and ranging capabilities, making it ideal for aerospace, mechanical control, exploration, marine, and port applications.

Key Features

  • Three-axis quartz MEMS gyroscope and accelerometer
  • High-precision single-antenna GNSS module
  • Integrated signal processing and navigation software
  • High-precision differential positioning and orientation
  • High reliability for aerospace and industrial applications

Applications

AerospaceMechanical controlExplorationMarinePort applications

Technical Specifications

Key Technical Specifications

Power Supply Voltage
5 ± 0.2 V
Operating Current @12V
135 ± 10 mA
Weight
75 ± 5 g

Gyroscope Specifications

Measurement Range
±300 °/s
Scale Factor
1 ± 0.005 undefined
Scale Factor Nonlinearity
≤300 ppm
Scale Factor Repeatability
≤300 ppm
Scale Factor Asymmetry
≤300 ppm
Cross-Axis Sensitivity
≤0.005 undefined
Threshold / Resolution
≤0.01 °/s
Bias (Full Temperature)
±0.1 °/s
Bias Stability (Room Temp)
≤20 °/h
Bias Stability (Full Temp)
≤50 °/h
Bias Repeatability
≤10 °/h
Angular Random Walk
≤0.08 °/√h
Bias Instability (Allan Deviation)
≤2 °/h

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

Integrated Navigation Performance (with 1m GNSS baseline)

Heading Accuracy (Speed ≥ 5 m/s)
≤0.3 °
Attitude Accuracy (Pitch/Roll)
≤0.1 °
Velocity Accuracy
≤0.1 m/s
Horizontal Position Accuracy
≤3 m
Vertical Position Accuracy
≤5 m

System Measurement Ranges

Heading Measurement Range
0 ~ 360 (Clockwise 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 ℃

Key Technical Specifications

Power Supply Voltage
5 ± 0.2 V
Operating Current @12V
55 ± 10 mA
Weight
80 ± 5 g

Gyroscope Specifications

Measurement Range
±400 °/s
Scale Factor
1 ± 0.005 undefined
Scale Factor Nonlinearity
≤100 ppm
Scale Factor Repeatability
≤100 ppm
Scale Factor Asymmetry
≤100 ppm
Cross-Axis Sensitivity
≤0.005 undefined
Threshold / Resolution
≤0.01 °/s
Bias (Full Temperature)
±0.1 °/s
Bias Stability (Room Temp)
≤10 °/h
Bias Stability (Full Temp)
- °/h
Bias Repeatability
≤10 °/h
Angular Random Walk
≤0.08 °/√h
Bias Instability (Allan Deviation)
≤2 °/h

Accelerometer Specifications

Measurement Range
±40 g
Bias (Full Temperature)
±5 mg
Bias Stability (Room Temp)
≤0.2 mg
Bias Stability (Full Temp)
≤2 mg
Bias Repeatability
≤0.2 mg

Integrated Navigation Performance (with 1m GNSS baseline)

Heading Accuracy (Speed ≥ 5 m/s)
≤0.3 °
Attitude Accuracy (Pitch/Roll)
≤0.1 °
Velocity Accuracy
≤0.1 m/s
Horizontal Position Accuracy
≤3 m
Vertical Position Accuracy
≤5 m

System Measurement Ranges

Heading Measurement Range
0 ~ 360 (Clockwise 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 ℃
  1. [1]This series covers multiple variants (one specification block set per variant); figures differ by variant — confirm the exact variant at inquiry.
  2. [2]Integrated navigation performance is specified with a 1 m GNSS baseline; heading accuracy requires a speed of at least 5 m/s.
  3. [3]Full-temperature gyroscope bias stability for one variant is not listed in the public specification — request the full datasheet at inquiry.

Package Information

Technical Drawings

Quartz MEMS Navigation Module D-Q-JDW-HDTD80CJ11
Dimensions Drawingdimensions
Quartz MEMS Navigation Module D-Q-JDW-HDTD80CJ12
Dimensions Drawingdimensions

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Technical Documentation

Detailed documentation is shared directly with qualified B2B buyers after inquiry, under mutual confidentiality. Customer, supplier, and program information is never published.

Include the model number and your application in the inquiry form — an engineer will respond with the relevant documents.

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Datasheet (PDF)

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

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