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, promoting 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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SNC200A-B0
SNC200A-B0 is an Inertial Measurement Unit (IMU) based on Micro Mechanical Systems (MEMS) technology, equipped with high-performance MEMS gyroscopes and accelerometers, capable of outputting 3-axis angular velocity, 3-axis acceleration, 3-axis magnetometer, and temperature. SNC200A-B0 has high reliability and strong environmental adaptability. By matching different software, the product can be widely applied in fields such as autonomous driving, industry drones, motion communication, high-precision map acquisition, and stable platforms.
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SNC200A-F0
SNC200A-F0 is an Inertial Measurement Unit (IMU) based on Micro Mechanical Systems (MEMS) technology, equipped with high-performance MEMS gyroscopes and accelerometers, capable of outputting 3-axis angular velocity, 3-axis acceleration, 3-axis magnetometer, and temperature. SNC200A-F0 has high reliability and strong environmental adaptability. By matching different software, the product can be widely applied in fields such as autonomous driving, industry drones, motion communication, high-precision map acquisition, and stable platforms.
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SNC200G-C0
SNC200G-C0 is an Inertial Measurement Unit (IMU) based on Micro Mechanical Systems (MEMS) technology, equipped with high-performance MEMS gyroscopes and accelerometers, capable of outputting 3-axis angular velocity, 3-axis acceleration, 3-axis magnetometer, and temperature. SNC200G-C0 has high reliability and strong environmental adaptability. By matching different software, the product can be widely applied in fields such as autonomous driving and industrial drones.
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SNC100E-A0
SNC100E-A0 integrated navigation system is equipped with high-performance MEMS gyroscopes, accelerometers, and magnetometers, which can receive GNSS data internally and achieve multi-sensor fusion and integrated navigation calculation. When GNSS is invalid, it has AHRS and VG functions, as well as short-term inertial navigation capability. This product has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in industry unmanned aerial vehicle systems.
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300A-A0/B0
SNC300A-A0/B0 is equipped with cost-effective closed-loop fiber optic gyroscopes, accelerometers, and high-end GNSS receiver boards. It is achieved through multi-sensor fusion and navigation algorithm, meeting the precise measurement requirements for attitude, heading, and position information in applications such as medium and high-precision mobile measurement systems and large unmanned aerial vehicles.
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SNC300D-A0
SNC300D-A0 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-A0 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-A0
SNC300F-A0 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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SNC300G-A0
SNC300G-A0 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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SNC500D-A0/A1/B0
SNC500D-A0/A1/B0 three types of rotating modulation inertial navigation systems all include three-axis fiber optic gyroscopes, accelerometers, and GNSS receiver boards. They are implemented through multi-sensor fusion and rotating modulation navigation solution algorithms, providing high-precision attitude, velocity, and position information to the external, meeting high-precision measurement and control requirements.
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SNC500E-A0/A1/A2
SNC600A is a compact dual axis rotating micro-mechanical (MEMS) inertial navigation system with three capabilities of self-calibration, self-alignment, and self-detection, which is maintenance free throughout its entire life cycle. SNC600A has high reliability and strong environmental adaptability. By matching different software, the product can be widely used in fields of autonomous driving, UAV, unmanned ships, and underwater equipment.
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SNC600D-A0
SNC600D-A0 is an inertial/visual/satellite integrated navigation system that highly integrates visual odometry technology, rotating modulation inertial navigation technology, and array IMU technology, achieving low-cost autonomous navigation under satellite denial. The product can be widely used in composite wing drones, fixed wing drones, and multi-rotor drones.
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