| Sign In | Join Free | My xpandrally.com | 
 | 
Place of Origin : China
Brand Name : Liocrebif
Certification : GJB 9001C-2017
Price : 5000-25000CHY
MOQ : 1
Packaging Details : Wooden box/Cardboard box/Container
Delivery Time : 2-4 weeks
Payment Terms : T/T
Supply Ability : 10000
Model Number : LKF-MSU300
Dimensions : 5.6*5.6*3.85 cm
Color&Classification : LKF-MSU300
Brand : Liocrebif
Output format : RS422
Application : Guidance weapons operating in harsh mechanical/thermal conditions, UAV/vehicle/ship/boat attitude reference, Attitude control systems, Radar/infrared antenna stabilization platforms
Original Place : China
LKF-MSU300 High-Precision MEMS Inertial Measurement Unit (IMU) is a highly reliable and cost-effective six-axis MEMS inertial sensor module, designed for a broad range of navigation, control, and measurement applications—particularly in inertial navigation and attitude stabilization.
LKF-MSU300 supports custom hardware/software configurations to meet diverse user requirements. For specialized inertial navigation applications, the gyroscope can be upgraded to high-precision or high-dynamic MEMS gyros, ensuring optimal performance for different operational needs.
LKF-MSU300 IMU integrates high-performance MEMS gyroscopes and accelerometers within a standalone structure. The selected gyroscopes and accelerometers represent the leading edge of MEMS inertial technology, with 100% domestically sourced electronic components.
High-Precision Manufacturing /System Calibration Technology
The company has developed a series of key technologies during the R&D process to ensure the product's high performance. The system employs high-speed sampling, static error compensation (fine compensation for zero bias, scale factor, and misalignment across the full temperature range), and dynamic error compensation (e.g., coning and sculling errors) to deliver optimal performance in user applications.
Table 1 Performance Parameters Of LKF-MSU300
| Gyroscope | |
| Range (°/s) | ±400 | 
| Bias(°/h) | ≤2 | 
| Bias Stability (°/h, 10s smoothing) | ≤0.3 | 
| Bias Instability (°/h, ALLAN) | ≤0.02 | 
| Angular Random Walk (°/√h) | ≤0.015 | 
| Bias Repeatability (°/h) | ≤0.1 | 
| Scale Factor Nonlinearity (ppm) | ≤100 | 
| Bandwidth (Hz) | ≥200 | 
| Cross-Coupling (rad) | ≤0.001 | 
| Resolution (°/s) | ≤0.001 | 
| Threshold (°/s) | ≤0.001 | 
| Accelerometer | |
| Range (g) | ±40 | 
| Bias (mg) | ≤2 | 
| Bias Stability (μg) | ≤100 | 
| Bias Instability (μg, ALLAN) | ≤30 | 
| Velocity Random Walk (μg/√Hz) | ≤30(0.018mm/s/sqrt(h)) | 
| Bias Repeatability (μg) | ≤100 | 
| Scale Factor Nonlinearity (ppm) | ≤300 | 
| Bandwidth (Hz) | ≥200 | 
| Cross-Coupling (rad) | ≤0.001 | 
| Resolution (μg) | ≤100 | 
| Threshold (μg) | ≤100 | 
| Electrical/Mechanical Interface | |
| Power Supply (V) | 5±0.2V | 
| Power Consumption (W) | ≤2 | 
| Startup Time (s) | ≤2 | 
| Communication Interface | 2×RS-422 | 
| Update Rate (Hz) | 200(Customizable up to 1000) | 
| Dimensions (mm×mm×mm) | 56×56×38.5 | 
| Weight (g) | 236±5g | 
| Operating Environment | |
| Operating Temperature (°C) | -45~80 | 
| Storage Temperature (°C) | -55~85 | 
| Vibration (g, RMS) | 13 | 
| Shock (g) | 1000g/1ms (powered), | 
Table 2 Definition of electrical interface
| Pin | Definition | DB9 Definition | Connect to testing device | 
| 2 | RS422 Rx+ | DB9-M1 | RS422 Tx+ | 
| 7 | RS422 Rx- | DB9-M2 | RS422 Tx- | 
| 3 | RS422 Tx+ | DB9-M3 | RS422 Rx+ | 
| 8 | RS422 Tx- | DB9-M4 | RS422 Rx- | 
| 6 | GND | DB9-M5 | DC 5V | 
| 1 | POWER_IN | DB9-M6 | 
High-precision MEMS IMU
100% domestically sourced components
High performance, compact size, lightweight, low power consumption
Full-temperature calibration compensation (-45°C to +80°C)
1KHz high-speed sampling
Harsh mechanical environment resistance
Supports firmware online updates
Guidance weapons operating in harsh mechanical/thermal conditions
UAV/vehicle/ship/boat attitude reference
Attitude control systems
Radar/infrared antenna stabilization platforms
Fig. 1 Outline Structure Dimension Diagram


|   | 
| High Precision Mems Imu Unit 5.6*5.6*3.85cm For Attitude Control Systems Images | 
 Miniature MEMS Inertia Measuring Unit Inertial Measurement System RS422 For
                                                                                    
                        
                        
                        
                                                            Miniature MEMS Inertia Measuring Unit Inertial Measurement System RS422 For
                                                    
                        
                     MEMS Inertial Measurement Unit Imu Sensor Reliable Inertial Management Unit 4.48
                                                                                    
                        
                        
                        
                                                            MEMS Inertial Measurement Unit Imu Sensor Reliable Inertial Management Unit 4.48
                                                    
                        
                     High Dynamic MEMS Inertial Measurement Unit RS422 For Navigation
                                                                                    
                        
                        
                        
                                                            High Dynamic MEMS Inertial Measurement Unit RS422 For Navigation
                                                    
                        
                     Integrated MEMS Inertial Unit Long Term DC 5V For Flight Control
                                                                                    
                        
                        
                        
                                                            Integrated MEMS Inertial Unit Long Term DC 5V For Flight Control
                                                    
                        
                     MEMS Inertial Sense Imu Micro Inertial Measurement Unit Autonomous High Overload
                                                                                    
                        
                        
                        
                                                            MEMS Inertial Sense Imu Micro Inertial Measurement Unit Autonomous High Overload
                                                    
                        
                     High Reliability Mems Based Imu 2.24*2.23*1.37cm 6 Axis For Navigation
                                                                                    
                        
                        
                        
                                                            High Reliability Mems Based Imu 2.24*2.23*1.37cm 6 Axis For Navigation
                                                    
                        
                     RS422 Mems Imu Sensor IMU Inertial Measurement Unit High Accuracy
                                                                                    
                        
                        
                        
                                                            RS422 Mems Imu Sensor IMU Inertial Measurement Unit High Accuracy
                                                    
                        
                     High Performance MEMS Inertial Measurement Unit RS422 For Navigation
                                                                                        
                                                        
                        
                        
                        
                                                            High Performance MEMS Inertial Measurement Unit RS422 For Navigation