Surface micromachined out-of-plane permalloy actuator arrays are developed for controlling the rolling moment of a tail-less delta-wing. The actuator consists of a millimeter sized electroplated permalloy plate with supporting polysilicon beams and is driven by an external magnetic field. Large angular deflections and vertical deflections are demonstrated. The magnetic forces and flow loading involved in the flap operation is on the order of hundred's of μN. Wind-tunnel tests confirm that a rolling moment on the wing can be generated by the flap operation.
|出版狀態||Published - 1995 1月 1|
|事件||Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference - Amsterdam, Neth|
持續時間: 1995 1月 29 → 1995 2月 2
|Other||Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference|
|期間||95-01-29 → 95-02-02|
All Science Journal Classification (ASJC) codes