Out-of-plane permalloy magnetic actuators for delta-wing control

Chang Liu, Tom Tsao, Yu Chong Tai, Tzong-Shyng Leu, Chih Ming Ho, Wei Long Tang, Denny Miu

Research output: Contribution to conferencePaper

46 Citations (Scopus)

Abstract

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.

Original languageEnglish
Pages7-12
Number of pages6
Publication statusPublished - 1995 Jan 1
EventProceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference - Amsterdam, Neth
Duration: 1995 Jan 291995 Feb 2

Other

OtherProceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference
CityAmsterdam, Neth
Period95-01-2995-02-02

Fingerprint

Magnetic actuators
Actuators
Polysilicon
Wind tunnels
Magnetic fields

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Mechanical Engineering
  • Electrical and Electronic Engineering

Cite this

Liu, C., Tsao, T., Tai, Y. C., Leu, T-S., Ho, C. M., Tang, W. L., & Miu, D. (1995). Out-of-plane permalloy magnetic actuators for delta-wing control. 7-12. Paper presented at Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference, Amsterdam, Neth, .
Liu, Chang ; Tsao, Tom ; Tai, Yu Chong ; Leu, Tzong-Shyng ; Ho, Chih Ming ; Tang, Wei Long ; Miu, Denny. / Out-of-plane permalloy magnetic actuators for delta-wing control. Paper presented at Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference, Amsterdam, Neth, .6 p.
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abstract = "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.",
author = "Chang Liu and Tom Tsao and Tai, {Yu Chong} and Tzong-Shyng Leu and Ho, {Chih Ming} and Tang, {Wei Long} and Denny Miu",
year = "1995",
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note = "Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference ; Conference date: 29-01-1995 Through 02-02-1995",

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Liu, C, Tsao, T, Tai, YC, Leu, T-S, Ho, CM, Tang, WL & Miu, D 1995, 'Out-of-plane permalloy magnetic actuators for delta-wing control' Paper presented at Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference, Amsterdam, Neth, 95-01-29 - 95-02-02, pp. 7-12.

Out-of-plane permalloy magnetic actuators for delta-wing control. / Liu, Chang; Tsao, Tom; Tai, Yu Chong; Leu, Tzong-Shyng; Ho, Chih Ming; Tang, Wei Long; Miu, Denny.

1995. 7-12 Paper presented at Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference, Amsterdam, Neth, .

Research output: Contribution to conferencePaper

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T1 - Out-of-plane permalloy magnetic actuators for delta-wing control

AU - Liu, Chang

AU - Tsao, Tom

AU - Tai, Yu Chong

AU - Leu, Tzong-Shyng

AU - Ho, Chih Ming

AU - Tang, Wei Long

AU - Miu, Denny

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N2 - 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.

AB - 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.

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Liu C, Tsao T, Tai YC, Leu T-S, Ho CM, Tang WL et al. Out-of-plane permalloy magnetic actuators for delta-wing control. 1995. Paper presented at Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference, Amsterdam, Neth, .