Description
INS-4533-R10 is a high-performance and high-precision fiber-optic integrated navigation system developed by AIT for aviation surveying and mapping, unmannedaerial vehicles, sea- based and road-based fields. Builtin three-axis fiber optic gyroscope, three-axisaccelerometer, optional three-axis magnetic sensor,high-precision air pressure sensor, including a BD/ GPS/GLONASS three-mode receiver. It can measure thespeed, position, and attitude of the carrier, and out put the compensated angular rate, acceleration, magnetic field, air pressure, temperature and other information.
INS-4533-R10 is equipped with a brand-new integrated navigation sensor fusion algorithm engine, optimized for multi-path interference, which can well meet the needs of long-term, high-precision, and high-reliability navigation applications in urban and field complex environments. The product supports multiple external sensors such as GNSS/ odometer/ DVL/ barome tricaltimeter, and has excellent scalability. By using multi sensor data fusion technology to combine inertial measurement with satellite navigation, odometer information and other information, the system can beregional adaptability and robustness have been greatly improved.
INS-4533-R10 integrated navigation system uses tight coupling technology to closely combine high-precision,professional-grade, multi-channel, dual-antenna single frequency carrier phase and pseudo-range GPS receivers with high-precision optical fiber inertial measurement units. It has small size, light weight, and Features such as high performance.
