A third generation, highly monitored, micromachined quartz rate sensor for safety-critical vehicle stability control

被引：4

作者：

Madni, AM ^{[1
]}

Costlow, LE ^{[1
]}

机构：

[1] BEI Technol Inc, Sylmar, CA 91342 USA

来源：

2001 IEEE AEROSPACE CONFERENCE PROCEEDINGS, VOLS 1-7 | 2001年

关键词：

D O I：

10.1109/AERO.2001.931213

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A Quartz Rate Sensor (QRS) family based on the Coriolis effect is presented. The architecture is highly capable of detecting internal failures. The MEMS solid-state rate gyro (known by the trade name GyroChip (R)) consists of a third generation microminiature double-ended quartz tuning fork, as well as third generation electronics in the form of a mixed signal ASIC. The high reliability device has no wearout mechanisms and features a micromachined sensing element. The sensor requirements, theory of operation, architecture, packaging family and performance parameters are described. In addition. system safety considerations and a description of the comprehensive self-monitoring features are provided.

引用

页码：2523 / 2534

页数：12

共 6 条

[1]

COSTLOW L, 2000, P SENS EXP DETR MICH, P53

[2]

Florida A.V., 1995, U.S. Patent, Patent No. [5,426,970, 5426970]

[3]

Madni AM, 1998, 1998 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS - PROCEEDINGS, VOLS 1-3, P1389, DOI 10.1109/IROS.1998.724782

[4]

Madni AM, 1996, 1996 IEEE AEROSPACE APPLICATIONS CONFERENCE, PROCEEDINGS, VOL 2, P315, DOI 10.1109/AERO.1996.495986

[5]

MADNI AM, 1999, J APPL SENSING T AUG, V16, P26

[6]

MADNI AM, 1997, P ITSC 97 IEEE C INT

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