AUTONOMOUS UNMANNED AIRCRAFT SYSTEM FOR THE GEOMETRICALLY IRREGULAR SURFACES SAMPLING: FATIGUE ANALYSIS AND DESIGN

Abstract

Here is registered as a guide a quad-copter design procedure, which is framed on implement a new movement aircraft methodology. This new approach break the classical kinematic displacement approaches, giving the quad-copter the capacity of realize partial on-fly inclinations. This without affecting its global position, velocity or acceleration values. All above focused in improve the general multi-rotor abilities into the autonomous sampling process. Clearly related with the irregular surfaces analyse, usually seen on the precision farming or simply on natural environments. A division has suggested to expose the step by step design cycle of two crucial mechanisms, first a tubular T-form quadcopter arm and second a central transformation mechanism. Both provide the reader a greater understanding about a whole and extensive airship design process. Each of the around ten integrated pieces are completely organized, easily raised and also correctly justified fulfilling the three point eight general security factor.

Keywords

• design; quad copter; fatigue; transformation; sampling