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Compact Quartz MEMS AHRS (Attitude and Heading Reference)

Attitude and Heading Reference System (AHRS) · ZHYS70CJ10

Compact attitude and heading reference system combining a six-axis quartz MEMS IMU (±300 °/s gyroscopes, 10 g accelerometers) with a three-axis magnetic sensor. Heading accuracy ≤2 °, pitch/roll attitude accuracy ≤0.5 °, 20 g class, −45 °C to +85 °C, suited to gimbals and ground or underwater platforms.

Attitude & Heading PerformanceHeading Accuracy
≤2 °
Attitude & Heading PerformanceAttitude Accuracy (Pitch/Roll)
≤0.5 °
Gyroscope SpecificationsMeasurement Range
±300 °/s
Read full specifications and measurement conditions ↓
Compact Quartz MEMS AHRS (Attitude and Heading Reference)
ZHYS70CJ10Product reference

Confirm configuration, interfaces and documentation with your inquiry.

The ZHYS70CJ10 is a compact, cost-effective attitude and heading reference system (AHRS), composed of a high-precision six-axis quartz MEMS inertial measurement unit, a three-axis high-precision magnetic sensor, and signal processing circuits. It provides accurate attitude information of the carrier and is well suited for industrial equipment, camera and antenna gimbals, as well as ground and underwater platforms.

Key Features

  • Six-axis quartz MEMS IMU + three-axis magnetic sensor
  • Accurate attitude and heading information
  • Compact and cost-effective
  • Suitable for industrial, gimbal, and platform applications

Applications

Industrial equipmentCamera and antenna gimbalsGround platformsUnderwater platforms

Technical Specifications

Key Technical Specifications

Power Supply Voltage
5 ± 0.2 V
Operating Current
40 mA
Weight
20 ± 5 g

Gyroscope Specifications

Measurement Range
±300 °/s
Scale Factor
1 ± 0.005
Scale Factor Nonlinearity
≤100 ppm
Scale Factor Repeatability
≤200 ppm
Scale Factor Asymmetry
≤200 ppm
Cross-Axis Sensitivity
≤0.005
Threshold / Resolution
≤0.01 °/s
Bias (Full Temperature)
±0.1 °/s
Bias Stability (Room Temp)
≤10 °/h
Bias Stability (Full Temp)
≤20 °/h
Bias Repeatability
≤10 °/h
Angular Random Walk
≤0.08 °/√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)
±10 mg
Bias Stability (Room Temp)
≤0.2 mg
Bias Stability (Full Temp)
≤2 mg
Bias Repeatability
≤0.4 mg

Attitude & Heading Performance

Heading Accuracy
≤2 °
Attitude Accuracy (Pitch/Roll)
≤0.5 °

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 ℃

Frequently Asked Questions

What is ZHYS70CJ10?+

Compact attitude and heading reference system combining a six-axis quartz MEMS IMU (±300 °/s gyroscopes, 10 g accelerometers) with a three-axis magnetic sensor. Heading accuracy ≤2 °, pitch/roll attitude accuracy ≤0.5 °, 20 g class, −45 °C to +85 °C, suited to gimbals and ground or underwater platforms.

Which specifications are published for ZHYS70CJ10?+

Key Technical Specifications — Power Supply Voltage: 5 ± 0.2 V; Key Technical Specifications — Operating Current: 40 mA; Key Technical Specifications — Weight: 20 ± 5 g. See the technical specifications for the complete parameter list.

Related Products

Supporting information

Documentation,
matched to your project.

Detailed documentation is shared directly with qualified B2B buyers after inquiry, under mutual confidentiality. Include the model and your application.

  • Datasheet (PDF)

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

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