High Accuracy Integrated Inertial Navigation System with Built-in MEMS gyroscope and accelerometer
Product Description
INS100C-C0 integrated navigation system has built-in high performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation algorithm, and have short-term inertial navigation capability when GNSS is invalid.
The product has high reliability and strong environmental adaptability. By matching different software, the products can be widely used in the fields of tactical and industrial unmanned aerial vehicles, unmanned vehicles, unmanned ships, aviation guided bombs, intelligent ammunition, rockets, mobile communication, mapping, seeker and stable platform.
Main Function
The integrated navigation system can use the satellite navigation information received internally to carry out integrated navigation, and output the information of the carrier, such as pitch, roll, heading, position, speed, time and the like; After losing the satellite signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain navigation accuracy maintenance function in a short time.
Technical parameters
| Project | Metrics (RMS) | Remark |
| | Dual GNSS | 0.1° | 2m baseline |
| Single GNSS | 0.1° | |
| Maintain accuracy | ≤0.3° | GNSS failure 0.5h |
| | GNSS is valid | 0.05° | |
| Maintain accuracy | ≤0.3° | GNSS failure 0.5h |
Horizontal positioning accuracy | | 1.2m | Single point L1/L2 |
| 2cm+1ppm | RTK |
| Maintain accuracy | ≤1nm | GNSS failure 10min |
Horizontal velocity accuracy | | | |
| | Measuring range | ±450°/s | |
| Zero bias stability | ≤0.5°/h | 10 s average |
| | Measuring range | ±16g | |
| Zero bias stability | ≤100µg | 10 s average |
| | | | |
| RS422 | Route 1 | |
Electrical characteristics | Voltage | 9~36VDC | |
| Power consumption | ≤6W | |
| Ripple | 100 mV | P-P |
Structural characteristics | Size | 80 mm×60mm×38mm | |
| Weight | ≤200g | |
| | Operating temperature | -40℃~+60℃ | |
| Storage temperature | -45℃~+70℃ | |
| Vibration | 20~2000Hz,6.06g | |
| Impact | 30g,11ms | |
| | MTBF | 30000h | |
| Continuous working time | >24h | |
Outline Drawing
Detail Photo
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High Accuracy Integrated Inertial Navigation System with Built-in MEMS Gyroscope and Accelerometer Images
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