Abstract
In this paper we propose a trajectory control method for a MEMS falling object as shown in Figure 1. The MEMS falling object is consisted of two units, an autorotation part and a non-rotation part. The autorotation part keeps its attitude stable with the gyro-effect of the autorotation phenomenon. The non-rotation part keeps a non-rotation state by using the air breaking boards. This non-rotation part controls its falling trajectory and the scattering region. By using large falling objects, aerodynamics of the falling object was characterized, e.g. falling speed, rotational speed, etc. Then the MEMS falling object was designed considering with this aerodynamics. The MEMS falling object was fabricated with a method of the SU-8 multi-layer structure. A MEMS autorotation part whose wing length is 6mm in diameter rotates at 4,800 rpm in the wind-tunnel successfully.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the IEEE International Conference on Micro Electro Mechanical Systems (MEMS) |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 308-311 |
| Number of pages | 4 |
| Volume | 2015-February |
| Edition | February |
| DOIs | |
| Publication status | Published - 2015 Feb 26 |
| Event | 2015 28th IEEE International Conference on Micro Electro Mechanical Systems, MEMS 2015 - Estoril, Portugal Duration: 2015 Jan 18 → 2015 Jan 22 |
Other
| Other | 2015 28th IEEE International Conference on Micro Electro Mechanical Systems, MEMS 2015 |
|---|---|
| Country | Portugal |
| City | Estoril |
| Period | 15/1/18 → 15/1/22 |
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ASJC Scopus subject areas
- Electrical and Electronic Engineering
- Mechanical Engineering
- Condensed Matter Physics
- Electronic, Optical and Magnetic Materials
Cite this
Trajectory control of MEMS falling object fabricated by SU-8 multilayer structure. / Yamane, Hokuto; Nagasawa, Sumito.
Proceedings of the IEEE International Conference on Micro Electro Mechanical Systems (MEMS). Vol. 2015-February February. ed. Institute of Electrical and Electronics Engineers Inc., 2015. p. 308-311 7050950.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Trajectory control of MEMS falling object fabricated by SU-8 multilayer structure
AU - Yamane, Hokuto
AU - Nagasawa, Sumito
PY - 2015/2/26
Y1 - 2015/2/26
N2 - In this paper we propose a trajectory control method for a MEMS falling object as shown in Figure 1. The MEMS falling object is consisted of two units, an autorotation part and a non-rotation part. The autorotation part keeps its attitude stable with the gyro-effect of the autorotation phenomenon. The non-rotation part keeps a non-rotation state by using the air breaking boards. This non-rotation part controls its falling trajectory and the scattering region. By using large falling objects, aerodynamics of the falling object was characterized, e.g. falling speed, rotational speed, etc. Then the MEMS falling object was designed considering with this aerodynamics. The MEMS falling object was fabricated with a method of the SU-8 multi-layer structure. A MEMS autorotation part whose wing length is 6mm in diameter rotates at 4,800 rpm in the wind-tunnel successfully.
AB - In this paper we propose a trajectory control method for a MEMS falling object as shown in Figure 1. The MEMS falling object is consisted of two units, an autorotation part and a non-rotation part. The autorotation part keeps its attitude stable with the gyro-effect of the autorotation phenomenon. The non-rotation part keeps a non-rotation state by using the air breaking boards. This non-rotation part controls its falling trajectory and the scattering region. By using large falling objects, aerodynamics of the falling object was characterized, e.g. falling speed, rotational speed, etc. Then the MEMS falling object was designed considering with this aerodynamics. The MEMS falling object was fabricated with a method of the SU-8 multi-layer structure. A MEMS autorotation part whose wing length is 6mm in diameter rotates at 4,800 rpm in the wind-tunnel successfully.
UR - http://www.scopus.com/inward/record.url?scp=84931073001&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84931073001&partnerID=8YFLogxK
U2 - 10.1109/MEMSYS.2015.7050950
DO - 10.1109/MEMSYS.2015.7050950
M3 - Conference contribution
VL - 2015-February
SP - 308
EP - 311
BT - Proceedings of the IEEE International Conference on Micro Electro Mechanical Systems (MEMS)
PB - Institute of Electrical and Electronics Engineers Inc.
ER -