高アスペクト比翼を有する無人航空機用飛行制御システムの安全性確認

抄録

This paper reports the safety confirmation of flight control system of an Unmanned Aerial Vehicle (UAV) with a pair of high-aspect-ratio wings via nonlinear simulations and hardware-in-the-loop simulation tests with various flight conditions (steady winds, gusts, etc.). The UAV successfully had a safe flight in Taiki town in Hokkaido after the safety confirmation process.