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TECHNOLOGICAL INNOVATION，NAVIGATING THE FUTURE
1 Years
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| Brand Name : | Liocrebif |
| Model Number : | LKF-MEMS Accelerometer |
| Certification : | GJB 9001C-2017 |
| Price : | 5000-25000CHY |
| Payment Terms : | T/T |
| Supply Ability : | 10000 |
| Delivery Time : | 2-4 weeks |
Introduction
MXD is a high-performance MEMS dual-axis accelerometer, independently developed by Liocrebif Technology with full localized production (ensuring supply control). It offers high-speed sampling, static/dynamic error compensation (full-temperature for zero drift, scale factor, installation errors) and correction algorithms, boasting excellent accuracy and stability in complex environments. Compact, easy to integrate, it fits space-constrained platforms, applicable to aerial surveying, inertial navigation, UAVs, robots, intelligent vehicles and bridge monitoring.
Technical Specification
Fully localized design with full-process control (core craftsmanship to packaging/testing) ensures supply stability and traceability. Integrated static/dynamic error compensation reduces zero offset and temperature drift, boosting accuracy and adaptability. Compliant with ISO9001 and GJB standards, ensuring consistent performance and high reliability in long-term use. System-level integration and optimization capabilities enable tailored solutions for diverse platforms, facilitating precise, efficient inertial navigation.
Table 1 Performance Parameters of LKF-MXD MEMS Accelerometer
Model | MXD05HC | MXD10HC | MXD16HC | MXD20HC | MXD30HC | MXD50HC | Unit |
Package | CLCC48 | CLCC48 | CLCC48 | CLCC48 | CLCC48 | CLCC48 | |
Axial | X,Y | X,Y | X,Y | X,Y | X,Y | X,Y | |
Range | 5 | 10 | 16 | 20 | 30 | 50 | g |
Scale nonlinearity | <1500 | <1500 | <1500 | <1500 | <1500 | <3000 | ppm(IEEE Norm , of full scale) |
Bandwidth (adjustable) 3db | 150 | 150 | 150 | 150 | 150 | 150 | Hz |
Delay | <1.5 | <1.5 | <1.5 | <1.5 | <1.5 | <1.5 | ms |
VRE | 100 | 100 | 50 | 50 | 40 | 30 | µg/g2 |
Noise | <12.5 | <15 | <20 | <25 | <40 | <100 | µg/√Hz |
Resolution | <12.5 | <15 | <20 | <25 | <40 | <100 | µg |
Pre-Shipment Bias (Room Temperature) | <±1 | <±1 | <±1 | <±1 | <±1 | <±1.5 | mg(Room temperature calibration value) |
Pre-Shipment Bias Temperature Drift | <±1.25 | <±2.5 | <±3 | <±3 | <±5 | <±6 | mg |
Pre-Shipment Bias Temperature Hysteresis | <0.2 | <0.4 | <0.5 | <0.5 | <0.6 | <0.7 | mg |
Post-Shipment Bias Compensation Residual | <±0.2 | <±0.25 | <±0.3 | <±0.4 | <±0.75 | <±1 | mg(Second-order piecewise compensation) |
Bias Stability 1s smooth | 13 | 20 | 25 | 25 | 50 | 100 | ug |
Bias Stability 10s smooth | 8 | 15 | 15 | 15 | 35 | 50 | ug |
Bias Stability allan | 2 | 4 | 5 | 5 | 10 | 15 | ug |
Yearly repeatability | <±0.6 | <±1 | <±1.25 | <±1.25 | <±1.75 | <±2 | mg |
Switching Repeatability 1σ | 5 | 7.5 | <10 | <10 | <20 | <20 | ug |
Factory-set Scale Factor | 1600000±320 | 800000±80 | 500000±50 | 400000±40 | 250000±50 | 150000±30 | Lsb/g(Room temperature calibration value) |
Yearly repeatability | <±250 | <±250 | <±250 | <±250 | <±250 | <±250 | Ppm |
Scale temperature coefficient | <80 | <80 | <80 | <80 | <80 | <80 | ppm/℃ |
Residual Error of Scale Factor after System Temperature Compensation | <100 | <100 | <100 | <100 | <100 | <100 | ppm(Second-order compensation) |
Start-up time | <0.5 | <0.5 | <0.5 | <0.5 | <0.5 | <0.5 | s |
Sampling frequency (adjustable) | 16K±5% | 16K±5% | 16K±5% | 16K±5% | 16K±5% | 16K±5% | Hz |
Electric shock | 3000 | 3000 | 3000 | 3000 | 6000 | 6000 | g |
No electrical shock | 3000 | 3000 | 3000 | 3000 | 6000 | 6000 | g |
Vibration rectification error (6 grms) | 1 | 1 | 1 | 0.5 | mg/grms | ||
Working temperature | -45-+85 | -45-+85 | -45-+85 | -45-+85 | -45-+85 | -45-+85 | ℃ |
Supply voltage | 5±0.25 | 5±0.25 | 5±0.25 | 5±0.25 | 5±0.25 | 5±0.25 | V |
Current | <20 | <20 | <20 | <20 | <20 | <20 | ma |
CI | SPI | SPI | SPI | SPI | SPI | SPI | SPI |
Main Features
100% localization of electronic components
Small volume packaging
High precision, wide range, and resistance to large impacts
Wide applicable temperature range
Full digital output
Application
Inertial Measurement Unit (IMU)
Aviation Electronics
Attitude control
Platform stability system
GPS assisted navigation
Unmanned aerial vehicle navigation system
Robots
North search and sonar positioning
Ship Navigation and Control
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