TY - JOUR
T1 - On improving the performance of a triaxis vortex convective gyroscope through suspended silicon thermistors
AU - Chang, Honglong
AU - Gong, Xianghui
AU - Wang, Shasha
AU - Zhou, Pingwei
AU - Yuan, Weizheng
N1 - Publisher Copyright:
© 2001-2012 IEEE.
PY - 2015/2/1
Y1 - 2015/2/1
N2 - This paper reports on a triaxis vortex convective gyroscope, in which a suspended arch-shaped silicon thermistor is proposed to improve performance by reducing the thermal-induced stress and heat dissipation to the substrate. The arch structure of the thermistor reduced the thermal-induced stress up to 88.7% compared with the clamped-clamped structure of the thermistor in our previous study. The suspended state reduced the heat dissipation to the substrate up to 32%. The experimental test results indicated that the sensitivities of the sensor for the x-axis, y-axis, and z-axis gyroscope were 0.642, 0.528, and 0.241 mV/°/s, respectively. The sensitivity improvement reached 49.65%, 56.21%, and 51.57% for each axis. The measured nonlinearity for the x-axis, y-axis, and z-axis gyroscope were 2.1%, 3.8%, and 4.5% in the range of ±100 °/s, respectively. An improvement in the linearity of 23.53%, 36.67%, and 6.25% was obtained.
AB - This paper reports on a triaxis vortex convective gyroscope, in which a suspended arch-shaped silicon thermistor is proposed to improve performance by reducing the thermal-induced stress and heat dissipation to the substrate. The arch structure of the thermistor reduced the thermal-induced stress up to 88.7% compared with the clamped-clamped structure of the thermistor in our previous study. The suspended state reduced the heat dissipation to the substrate up to 32%. The experimental test results indicated that the sensitivities of the sensor for the x-axis, y-axis, and z-axis gyroscope were 0.642, 0.528, and 0.241 mV/°/s, respectively. The sensitivity improvement reached 49.65%, 56.21%, and 51.57% for each axis. The measured nonlinearity for the x-axis, y-axis, and z-axis gyroscope were 2.1%, 3.8%, and 4.5% in the range of ±100 °/s, respectively. An improvement in the linearity of 23.53%, 36.67%, and 6.25% was obtained.
KW - Gyroscope
KW - MEMS.
KW - heat conduction losses
KW - thermal-induced stress
KW - thermistors
UR - https://www.scopus.com/pages/publications/84915819065
U2 - 10.1109/JSEN.2014.2358700
DO - 10.1109/JSEN.2014.2358700
M3 - 文章
AN - SCOPUS:84915819065
SN - 1530-437X
VL - 15
SP - 946
EP - 955
JO - IEEE Sensors Journal
JF - IEEE Sensors Journal
IS - 2
M1 - 6901238
ER -