折りたたみ機構を有する羽ばたき翼の研究

抄録

Because of the recent development of science and technology, Micro Air Vehicle (MAV) has been advanced to the investigation, such as a disaster site. These aircraft have spread, in this condition there is a possibility of contact with an obstacle when moving on the ground. For damage to the power source is fatal to MAV, we consider that the development of the folding mechanism is an urgent need, in the present study was carried out its development.