Space Navigation and Control
Beijing Space Navigation and Control Technology Co., Ltd. (SNC) is a modern high-tech enterprise integrating research and development and production of inertial navigation, focusing on the R&D, production and sales of inertial devices, inertial measurement units and integrated navigation systems. The company's products have been successfully applied in the fields of UAV, smart mines, autonomous driving, surface and underwater applications，surveying and mapping, and have provided products and services to customers such as research institutes, key universities, and high-tech enterprises. The company has technological leadership in the overall design, algorithm design, software and hardware design of inertial products, and has formed a multi-professional technical research and development team, always maintaining the concept of technological innovation, helping the company to maintain innovation，progressiveness and competitiveness in the field of inertial navigation.
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Beautiful Harmonious
PRODUCT CENTER
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SNC100C-A0
SNC100C-A0 integrated navigation system has high-performance MEMS gyro and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation algorithm, and provide short-term inertial navigation capability when GNSS is invalid. The product has high reliability and strong environmental adaptability.
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SNC100C-B0
SNC100C-B0 integrated navigation system has high-performance MEMS gyro and accelerometer. This system can receive internal GNSS data, realize multi-sensor fusion and integrated navigation algorithm. When GNSS is invalid, the position, speed and attitude of inertial solution can be output, and certain navigation accuracy can be maintained in a short time. In the integrated navigation, it can output the original post-processing information for NovAtel's IE post-processing software.
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SNC100E
SNC100E integrated navigation system has high-performance MEMS gyro and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation algorithm, and provide short-term inertial navigation capability when GNSS is invalid. The product has high reliability and strong environmental adaptability.
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SNC300A
SNC300A is based on cost-effective closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board. By realizing multi-sensor fusion and navigation algorithm. SNC300A-A0 can meet the precise measurement requirements
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SNC300C
SNC300C is a compact INS with FOG and MEMS accelerometer. It can use accurate timing and positioning information of external GNSS to carry out inertial/satellite integrated navigation. When external GNSS is invalid, the INS has high precision
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SNC300D
SNC300D is based on cost-effective closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board. By realizing multi-sensor fusion and navigation algorithm. SNC300D can meet the precise measurement requirements of attitude, heading and position in medium-high precision mobile measurement systems and large unmanned aerial vehicles.
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SNC300F
SNC300F is a compact inertial navigation system using fiber optic gyroscopes, which integrates GNSS dual antenna board internally and can perform inertial/satellite integrated navigation. When GNSS information is invalid, inertial navigation has a high ability to maintain pure inertial navigation accuracy.
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SNC500A
SNC500A fiber integrated navigation system is based on high-precision closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board, through multi-sensor fusion and rotation modulation navigation solution algorithm, to provide high-precision attitude, speed and position, to meet the requirements of high-precision measurement and control.
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