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

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

^*Corresponding author for this work

Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

50 Scopus citations

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 language	English (US)
Title of host publication	Proceedings of the IEEE Micro Electro Mechanical Systems
Editors	Anon
Publisher	IEEE
Pages	7-12
Number of pages	6
State	Published - Jan 1 1995
Event	Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference - Amsterdam, Neth Duration: Jan 29 1995 → Feb 2 1995

Other

Other	Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference
City	Amsterdam, Neth
Period	1/29/95 → 2/2/95

ASJC Scopus subject areas

Control and Systems Engineering
Mechanical Engineering
Electrical and Electronic Engineering

Cite this

@inproceedings{514f03d80d4b445cbd963e0e9118f5d3,

title = "Out-of-plane permalloy magnetic actuators for delta-wing control",

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 Leu, {Tzong Shyng} and Ho, {Chih Ming} and Tang, {Wei Long} and Denny Miu",

year = "1995",

month = jan,

day = "1",

language = "English (US)",

pages = "7--12",

editor = "Anon",

booktitle = "Proceedings of the IEEE Micro Electro Mechanical Systems",

publisher = "IEEE",

note = "Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference ; Conference date: 29-01-1995 Through 02-02-1995",

}

TY - GEN

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

PY - 1995/1/1

Y1 - 1995/1/1

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.

UR - http://www.scopus.com/inward/record.url?scp=0029180835&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0029180835&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:0029180835

SP - 7

EP - 12

BT - Proceedings of the IEEE Micro Electro Mechanical Systems

A2 - Anon, null

PB - IEEE

T2 - Proceedings of the 1995 IEEE Micro Electro Mechanical Systems Conference

Y2 - 29 January 1995 through 2 February 1995

ER -

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

Abstract

Other

ASJC Scopus subject areas

Other files and links

Fingerprint

Cite this