A Miniature Integrated Navigation System for Rotary-Wing Unmanned Aerial Vehicles

A Miniature Integrated Navigation System for Rotary-Wing Unmanned Aerial Vehicles

This paper presents the development of a low cost miniature navigation system for autonomous flying rotary-wing unmanned aerial vehicles (UAVs). The system incorporates measurements from a low cost single point GPS and a triaxial solid state inertial/magnetic sensor unit. The navigation algorithm is...

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Bibliographic Details
Main Authors: Yu Xu, Wenda Sun, Ping Li
Format: Article
Language:English
Published: Wiley 2014-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2014/748940
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