| Color&Classification | LKF-MSU203 |
| Original Place | China |
| Brand | Liocrebif |
| Dimensions | 4.48*3.86*2.15cm |
| Application | Radar/infrared antenna stabilization platforms, UAV attitude reference/flight path control, Missile flight control Vehicle/ship attitude measurement, Port measurement systems, Satellite communication on-the-move, Drilling and extraction systems, Mobile ma |
| Output format | RS422 |
| Payment Terms | T/T |
| Supply Ability | 10000 |
| Delivery Time | 2-4 weeks |
| Packaging Details | Wooden box/Cardboard box/Container |
| Brand Name | Liocrebif |
| Model Number | LKF-MSU203 |
| Certification | GJB 9001C-2017 |
| Place of Origin | China |
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Product Specification
| Color&Classification | LKF-MSU203 | Original Place | China |
| Brand | Liocrebif | Dimensions | 4.48*3.86*2.15cm |
| Application | Radar/infrared antenna stabilization platforms, UAV attitude reference/flight path control, Missile flight control Vehicle/ship attitude measurement, Port measurement systems, Satellite communication on-the-move, Drilling and extraction systems, Mobile ma | Output format | RS422 |
| Payment Terms | T/T | Supply Ability | 10000 |
| Delivery Time | 2-4 weeks | Packaging Details | Wooden box/Cardboard box/Container |
| Brand Name | Liocrebif | Model Number | LKF-MSU203 |
| Certification | GJB 9001C-2017 | Place of Origin | China |
| High Light | MEMS Inertial Measurement Unit Imu Sensor ,MEMS Inertial Management Unit ,Reliable Inertial Management Unit | ||
MOQ: 1
Size: L(4.48) × W(3.86) × H(2.15) cm
Specification Number: LKF-MSU203
| Parameter | Technical Index |
|---|---|
| Gyroscope | |
| Measurement Range (°/s) | ±500 |
| Full-Temperature Bias (°/h, 3σ) | ≤30 |
| Bias Stability (°/h, 10s averaging window) | ≤2 |
| Bias Instability (°/h, Allan variance, typical) | ≤0.1 |
| Bias Repeatability (°/h) | ≤1 |
| Angular Random Walk (°/√h) | ≤0.1 |
| Scale Factor Nonlinearity (ppm) | ≤100 |
| Cross-Coupling Error (rad) | ≤0.001 |
| Bandwidth (Hz) | ≥200 Hz |
| Accelerometer | |
| Measurement Range (g) | ±30 |
| Full-Temperature Bias (mg, 3σ) | ≤2 |
| Bias Stability (μg, 10s averaging window) | ≤50 |
| Bias Instability (μg, Allan variance, typical) | ≤30 |
| Bias Repeatability (μg) | ≤50 |
| Velocity Random Walk (m/s/√h) | ≤0.03 |
| Scale Factor Nonlinearity (ppm, ±1g input) | ≤100 |
| Cross-Coupling Error (rad) | ≤0.001 |
| Bandwidth (Hz) | ≥200 Hz |
| Physical Characteristics | |
| Supply Voltage (V) | 5~12 (ripple ≤100 mV) |
| Steady-State Power Consumption (W) | ≤2 |
| Startup Time (s) | ≤2 |
| Maximum Data Update Rate (Hz) | 2000 |
| Overall Dimension (mm×mm×mm) | 44.8×38.6×21.5 |
| Weight (g) | 52±5 |
| Operating Environment | |
| Operating Temperature (℃) | -40 ~ 80 |
| Storage Temperature (℃) | -55 ~ 85 |
| Vibration (g, RMS, 20~2000 Hz) | 6.06 |
| Shock (g, 1 ms half-sine pulse) | 500 |
| Pin No. | Definition | Remarks |
|---|---|---|
| 8 | POWER_IN | Power supply range: 5 V ~ 12 V (output ripple ≤ 100 mV) |
| 15 | GND | |
| 6 | RS232_TXD1 | RS232 communication interface |
| 5 | RS232_RXD1 | |
| 3 | GND | |
| 10 | RS422 R+ | M1: RS422 communication interface |
| 2 | RS422 R- | |
| 9 | RS422 T+ | |
| 1 | RS422 T- | |
| 14 | RS232_TXD2 | M2: RS232 communication interface, supports external GNSS module input for timestamp tagging |
| 7 | RS232_RXD2 | |
| 13 | GND | |
| 11 | PPS_IN | |
| 4 | TOV | General-purpose IO port, 3.3 V logic level, rising edge active |
| 12 | GND |
Company Details
Business Type:
Manufacturer,Exporter,Seller
Year Established:
2019
Total Annual:
6000000-7000000
Employee Number:
101~200
Ecer Certification:
Verified Supplier
COMPANY INTRODUCTION LIOCREBIF primarily engages in the research, development, production, and distribution of various inertial navigation systems, inertial measurement units, gyroscopes, and related products, providing specialized services in the fields of inertial navigation and optoelectronic sen... COMPANY INTRODUCTION LIOCREBIF primarily engages in the research, development, production, and distribution of various inertial navigation systems, inertial measurement units, gyroscopes, and related products, providing specialized services in the fields of inertial navigation and optoelectronic sen...
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