A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.
|出版ステータス||Published - 2006 11月 21|
|イベント||9th IEEE International Workshop on Advanced Motion Control, 2006 - Istanbul, Turkey|
継続期間: 2006 3月 27 → 2006 3月 29
|Conference||9th IEEE International Workshop on Advanced Motion Control, 2006|
|Period||06/3/27 → 06/3/29|
ASJC Scopus subject areas
- コンピュータ サイエンスの応用