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Inertial navigation systems (INS) are widely used for controlling piloted or unmanned aerial vehicles (UAV). Automatic control equipment with INS has error budget making a huge impact on the accuracy of UAV navigation. The paper analyzes INS errors and types of errors. Experiments have been done using small UAV

ERROR ANALYSIS OF INS ARRANGED IN ARDUPILOT MEGA / „ARDUPILOT MEGA“ AUTOPILOTO INERCINIO NAVIGACIJOS ĮRENGINIO PAKLAIDŲ ANALIZĖ