Research of the pendulum gravity control postural stabilization flight robot using dynamic inversion control

点击翻译按钮获取中文摘要

The design of an inclusion control circuit and the manufacture of an electric circuit which put into dynamic inversion control software were performed, and it built in the test prototype of 1/3 scale, and conducted the attitude control experiment of as opposed to aerial disturbance for an experiment. It became clear that the effect which controls rolling motion is reduced by combining angular velocity sensor (gyroscope sensor) feedback and the angular acceleration sensor of a high sampling frequency. Using these results, in the Niigata sky project, the research and development of the turbojet engine which is a lightweight body, development of the electric high thrust control actuator of 2 axes, and lightweight body using a carbon fiber composite material is developed, and a pendulum stable control type unmanned aerial vehicle is manufactured.Real application of the result of research is aimed at.