In-Flight Alignment of a Strapdown Inertial Navigation System of an Unmanned Aerial Vehicle

摘要

The alignment system of a strapdown inertial navigation system for an unmanned aerial vehicle installed on a carrier aircraft is studied. The aim is to develop alignment techniques for the strapdown inertial navigation system that improve the accuracy of alignment and reduce the alignment time. A technique for constructing the initial alignment system fora strapdown inertial navigation system of an unmanned aerial vehicle is proposed.