INS Alignment

The objective of this project is to implement the alignment algorithms for an Inertial Navigation System (INS). These algorithms are used to define the position and orientation of an aircraft or stabilized platform before take-off or operation. The algorithms to be implemented consist of the static alignment, transfer alignment and in-flight alignment of the INS. The algorithms are to be implemented on an embedded microprocessor and tested using industrial guidelines.

This project will run as a 4th year Electronic Engineering project during 2008.