Integrated navigation processing equipment for launch reference is used to provide accurate, continuous and smooth navigation reference information for missile alignment. It can receive multiple sets of inertial navigation equipment data to complete functions such as synchronization, smoothing, redundant monitoring and diagnosis of multiple inertial navigation data information; it can send dual redundant synchronization 422, dual redundant Gigabit to control stations, launch management equipment, etc. High real-time baseline navigation data such as Ethernet and dual-redundant optical fiber Ethernet. It has the characteristics of high precision, strong versatility and high reliability, and can meet the application needs of many types of launch platforms such as ships, vehicles and containers.

• Provide launch benchmark information in real time. The continuous working time after one power-on exceeds 120h; redundant inertial navigation data diagnosis and isolation time is less than 5ms; synchronization information time delay is not greater than 0.1ms
• Strong versatility. Adopts standard 3U/4U chassis design to facilitate user product configuration
• Domestic production is independent and controllable. Using domestic Loongson 3A3000 processor and solid state drive
• The interface has strong scalability. Provides dual redundant synchronous 422, dual redundant Gigabit Ethernet, dual redundant optical fiber Ethernet and other interfaces to meet the application needs of different transmission systems
• Strong environmental adaptability, can meet the vibration, impact and temperature environment of various launch platforms

Land use, navigation, drones, and can also be extended to other applications.