This thesis investigates possibility to improve reliability and performance of low-cost aeronautical integrated navigation systems by making use of robust autonomous measurements, namely of inertial measurement unit, air data system, and 3-axis magnetometer. The central applied result of the research consists in proposing low size, weight, power, and cost design of a robust platform-autonomous fault-tolerant navigation system with the best in-IMU-class performance, which, in the events of failures, can gracefully degrade to attitude and heading reference system.      «

This thesis investigates possibility to improve reliability and performance of low-cost aeronautical integrated navigation systems by making use of robust autonomous measurements, namely of inertial measurement unit, air data system, and 3-axis magnetometer. The central applied result of the research consists in proposing low size, weight, power, and cost design of a robust platform-autonomous fault-tolerant navigation system with the best in-IMU-class performance, which, in the events of failur...     »