Software in Loop Simulation based Waypoint Navigation for Fixed Wing UAV

Software in loop simulation (SILS) based waypoint navigation test platform being presented this paper for fixed wing unmanned aerial vehicle. The proposed helps to algorithm before implementing into real time environment. Matlab/Simulink and X-plane flight simulator are chosen the platform. interface between these two platforms done by using user datagram protocol (UDP). which is be tested run environment where as model runs simulator. Inverted T tail vehicle configuration research work verify both its inner (attitude control) outer (navigation control). Navigation executed compares difference current desired latitude longitude position command reach waypoint. towards a will achieved varying attitude of an Finally results observed performances verified