PRECISION ACCELEROMETERS WITH MU-G RESOLUTION

被引:75
作者
RUDOLF, F
JORNOD, A
BERGQVIST, J
LEUTHOLD, H
机构
[1] Centre Suisse d'Electronique et de Microtechnique S.A.
关键词
D O I
10.1016/0924-4247(90)85059-D
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
A highly miniaturized accelerometer for micro- gravity measurements in spacecraft has been developed. It is based on a capacitive micromechanical silicon chip and an associated CMOS measurement integrated circuit. The accelerometer has been modeled in order to select and to optimize the system. The technology for the electromechanical chip, based on a glass-silicon sandwich structure has been developed. The final accelerometer developed, with an analog output signal of 5 V/g and a working range of ± 0.1 g, has a resolution of less than 1 μg at 1 Hz. Transverse sensitivities are below 0.4%. The temperature coefficients of offset and sensitivity are typically 30 μg/°C and 150 ppm/ °C respectively. Bandwidth is d.c. to 100 Hz. The hybrid technique accelerometer package has a size of 33 mm × 15 mm × 5 mm. © 1990.
引用
收藏
页码:297 / 302
页数:6
相关论文
共 10 条
[1]  
BARTH P, 1988, JUN SOL STAT SENS AC
[2]  
LEFORT O, 1989, JUN P CAPT 89 PAR, P313
[3]   AN ASIC FOR HIGH-RESOLUTION CAPACITIVE MICROACCELEROMETERS [J].
LEUTHOLD, H ;
RUDOLF, F .
SENSORS AND ACTUATORS A-PHYSICAL, 1990, 21 (1-3) :278-281
[4]  
ROARK RJ, 1985, FORMULAS STRESS STRA
[5]   A MICROMECHANICAL CAPACITIVE ACCELEROMETER WITH A 2-POINT INERTIAL-MASS SUSPENSION [J].
RUDOLF, F .
SENSORS AND ACTUATORS, 1983, 4 (02) :191-198
[6]  
RUDOLF F, 1987, 4TH INT C SOL STAT S, P395
[7]  
SANDMAIER H, 1987, 4TH INT C SOL STAT S, P399
[8]  
SEIDEL H, 1989, MIKROMECHANIK HEIDEL, P147
[9]  
TSUGAI M, 1987, 4TH INT C SOL STAT S, P403
[10]   INTERFACE CIRCUIT FOR CAPACITIVE ACCELEROMETER [J].
VANPAEMEL, M .
SENSORS AND ACTUATORS, 1989, 17 (3-4) :629-637