Design of an Autonomous GPS/INS Navigation System for Guided Bomb with Wing Adapter Kit

Inertial Navigation System-The report documents the development of algorithms for an inertial navigation system (INS). In general, inertial navigation consists of three parts: Alignment, navigation and aiding. Algorithms for these parts are d

This thesis is to investigate the integration of Precise Point Positioning GPS and low cost MEMS IMU. Both loosely and tightly coupled Kalman filters are developed to derive the optimal navigation solution.Global Positioning System (GPS) and lo