3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft

Product Details
Customization: Available
Type: Inertial Measurement Unit
Output Signal Type: Digital Output
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Registered Capital
1000000 RMB
Plant Area
>2000 square meters
  • 3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
  • 3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
  • 3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
  • 3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
  • 3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
  • 3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
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Basic Info.

Model NO.
IMU388
Measuring Shaft Quantities
6
Accuracy Grade
0.6degree/H
IP Rating
IP67
Certification
ISO
Customized
Non-Customized
Range
Gyro: +-500deg/S, Acc: +-40g
Bias Instability
Gyro: 0.6deg/H, Acc: 30ug
Working Temperature
-40~+85degc
Interface
Uart
Transport Package
Carton
Specification
33.5*25.5*15mm
Trademark
SkyMEMS
Origin
China
HS Code
9014100000
Production Capacity
2000/Month

Product Description

IMU388 Tactical 6DoF MEMS IMU

3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
Main Features
- High Precision Tactical 6DoF MEMS IMU Sensor
- Range 
(Typical): Gyro ±500°/s, Acc ±40g
- Bias Instability (Allan): Gyro: 0.6°/h, Acc 30μg
Strict Factory Calibration, Full Temp. Compensation
- High Bandwidth (Typical): 200Hz, RS422 Interface
Proven Reliability, Dependability and Ruggedness
- Compact Size: 33.5×25.5×15 mm
- Working Temperature: -40~+85°C

Brief Introduction

IMU388 is a high performance tactical grade MEMS Inertial Measurement Unit, which enjoys high accuracy: MEMS gyroscope is 0.6°/h bias instability (Allan) and MEMS accelerometer is 30µg bias instability (Allan), and its MEMS gyroscope range can be optional in ±250°/s~ ±4000°/s, the accelerometer range is ±40g, and it can output precise 3-axis outputs of angular rate and 3-axis acceleration data.

IMU388 adopts latest MEMS technology and advanced MEMS components, and it has been produced in bulk, which reduces the cost deeply. IMU388 can output precise measurement data in harsh environment, and it has been widely applied in unmanned aircraft, unmanned surface vessel, platform stabilization, industrial robotics, etc., and IMU388 is easily integrated into the variety of architectures that these applications present. The extremely small size, light weight, and low power make the IMU388 ideal for most applications.

Technical Specifications  
Parameter            Test Condition Min Typical Max Unit
Gyroscopes
  Range1     ±500   °/s
  Bias Instability Allan variance    0.6   °/h 
10s average (-40~+85°C, fixed temp.)   2   °/h
  Bias Repeatability     1.8   °/h 
  Radom Walk     0.1   º/√h
  Bais Bias change at full temp. range2   ±0.04   °/s
Bias change in vibration conditions3   6   °/h 
  Scale Factor Nonlinearity     100   ppm
  Bandwidth     200   Hz
Accelerometers
  Range1     ±40   g
  Bias Instability Allan variance    50   ug
10s average (-40~+85°C, fixed temp.)   100   ug
  Bias Repeatability     100   ug
  Random Walk     0.01   m/s/√h
  Non-linearity     100   ppm
  Bandwidth     200   Hz
Interface4(RS422)
    Baud Rate   115200 230400 921600 bps
    Output Rate   250 500 2000 Hz
Reliability
  MTBF   20000h
  Continuous Working Time   120h
Electronic Features
  Supply Voltage   3.6 ~ 36 V
  Power Consumption   < 0.2 W
  Ripple Wave    100mV (P-P)
Environment Conditions
  Operating Temperature   -40°C ~ 85°C
  Storage Temperature   -55°C ~ 105°C
  Vibration Resistance   20~2000Hz,  6.06g
  Shock Resistance   1000g,  0.5ms
Physical Characteristics
  Size   33.5 × 25.5 × 15 mm
  Weight   30grams
  Interface Model   9pins J63A
Note:
1:
The range of Gyroscopes and Accelerometers can be configured in our factory.
2: The bias value is calculated based on the whole temperature change period, the temperature changing rate<=2°C/minute,             temperature range:-40~+85°C;
3: (before vibration average value +after vibration average value) /2-during vibration average value, the vibration conditions are        6.06g, 20~2000Hz
4: The baud rate and output rate can be configured in our factory.


Typical Applications

- Airborne Optoelectronic Pod


- Target Drone

- Armored Personnel Carrier

- Rain-Seeding Rocket



Product Advantages

Why Selecting IMU388M Inertial Measurement Unit

IMU388M Inertial Measurement Unit is designed and produced by SkyMEMS, it enjoys high performance and accuracy, extra large range, and high reliability with competitive price. It is a tactical inertial measurement unit sensor, which has the main following advantages:

1. Extra Large Range, High Accuracy, High Performance and Powerful Functions
3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
IMU388M Inertial Measurement Unit is a precision 10 DoF MEMS inertial measurement unit, which enjoys excellent technical advantages:
  • High Precision Tactical 6DoF MEMS IMU Sensor
  • Range (Typical): Gyro ±500°/s,  Accel ±40g
  • Bias Instability (Allan): Gyro: 0.6°/h, Accel 30µg
  • Strict Factory Calibration, Full Temp. Compensation
  • High Bandwidth (Typical) : 200Hz, RS422 Interface
  • Proven Reliability, Dependability and Ruggedness
  • Compact Size: 33.5x25.5x15mm
  • Working Temperature: -40~+85°C
IMU388M Inertial Measurement Unit adopts big brand components, high-class glue encapsulation, advanced production craft, and fully calibrated, which assured that our products have real actual precise and perfect performance.

2. Aerospace Level Reliability, 12-step Strictest Quality Control
3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft

We have advanced product test team and measurement equipment, and we cherish the quality as the life of the company, all our products must pass the strictest quality control procedures, our unique 12-step quality control assures our products enjoy top level quality.

3. Competitive Price, ODM Supported
3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft
With strict cost control and massive production, we can provide the most competitive cost-effective prices, and we have abundant ODM service experience for customers around the world, that is why we can build up long term win-win cooperation with our customers.

4. Successful Applications in many Fields, 200+ Customers are Using

We are continuously focusing on MEMS measurement & control technologies. IMU388 has been widely used in tactical UAS Navigation & Control, Seeker, Platform Stabilization, etc. and now more than 200 customers are using our tactical IMU around the world.

5. World-class Production Line, Fast Delivery
3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft

We have the world class production line to assure that the production procedures are scientific, precise, and normative, which also can assure our products to be fast delivered.

6.Service with Heart, Professional Technical Support
3-Axis Acc+Gyro Advanced Inertial Navigation Measurement Unit Sensor for Unmanned Aircraft

We have the professional technical support engineer team, which can provide 24-hour technical support and excellent after-sale service.

Serving customers with heart is the principle of SkyMEMS, Customer demand is the fundamental driving force of our development.

We treat our customers with heart, customers' satisfaction is the direction and target of SkyMEMS. Through continuously technology innovation and service upgrading, we will realize win-win cooperation with customers.

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