Drift Correction in Inertial Navigation Systems

The I7100 micro-inertial navigation system primarily consists of MEMS gyroscopes, accelerometers, signal processing circuits, and satellite navigation modules. It is characterized by its compact size, lightweight, and low cost, making it suitable for various applications such as small and micro drones, mobile communication antennas, and electro-optical pods. The main features are as follows: → Dual-antenna heading alignment or moving base maneuvering alignment can be utilized → It features multiple working modes, including short-term pure inertial, inertial/satellite combination, inertial/vision combination, and horizontal attitude indicator → It possesses functions such as high-precision post-processing and heave measurement → Built-in multiple communication protocols, with configurable serial port baud rate and output protocol → Operating temperature: -45℃～+70℃ → It features multiple interfaces such as RS422, RS232, and PPS input/output → Power supply: 6V~36V, power consumption <2W → Weight: <70g → Size: 56mm×41mm×25mm

I3500 is an integrated navigation system (GNSS/INS) composed of high-performance MEMS sensors, high-precision GNSS systems and high-performance microprocessors.  The built-in self-developed high-reliability integrated navigation algorithm can output the speed, position, attitude and other information of the measured carrier in real time. Users can also externally connect RTCM differential correction data to achieve high-precision RTK positioning. The IP68 waterproof shell-type package can be easily integrated into the user's system. Product model information is as follows: