Synthesize of Design of Inertial navigation system (INS) using MEMS sensor

Abstract

The purpose of this project is mainly to convey an elementary inertial navigation system, and take advantage of the capabilities that the Micro-Electromechanical system (MEMS) affords. The main aspects cover the simplicity, intuition, and fairness in the design of inertial navigation system. A noticeable tendency of cutting-off the cost of materials and facilities that are used to design any system in general is in demand which stands no-distance from the intention behind designating this system. Thus, using MEMS sensor and Programmable microcontroller to emulate the inertial navigation system is quite affordable and stands for the expected performance. The information yielded from the sensor as real-time evaluation of the momentarily motion and deviation of the airplane is illustrated on a Liquid crystal display (LCD), as a fair and neat technique of showing upshot digitally. The outcome of the work achieved turns to stand up as simplified system for the sake of understanding and building of affordable and yet reliable system, although main components are not fully supported and a lot of restriction is applied, the final project was carried down but in longer time. Furthermore, the need of well understanding and studying of the inertial navigation system is considerable in order to get more familiarize with the Inertial navigation system.