DocumentCode :
1257655
Title :
Micro inertial measurement system from China
Author :
Dong, Haifeng ; Zhang, Wendong
Author_Institution :
Dept. of Electron. Eng., North China Inst. of Technol., Taiyuan, China
Volume :
5
Issue :
1
fYear :
2002
fDate :
3/1/2002 12:00:00 AM
Firstpage :
16
Lastpage :
19
Abstract :
The micro inertial measurement system (MIMS) integrates measurement, sampling, quantization, coding/compression, and storage. It can be used in the measurement of dynamic data in rockets, missiles, and vehicles. It can also monitor, collect, and record data from the human body and ambient environment, and then provide output to a hard disk through a computer interface. These data will later be used to analyze human health. MIMS, which comprises a micro electronic mechanical system (MEMS) transducer, a signal acquisition module, a data compression module, a control circuit, and memory can be used in a variety of applications with different environments and requirements. Volume, cost, and reliability are some of the design variables that we considered. Our research on the MIMS includes a single-chip accelerometer and angle-rate transducer, a novel attitude algorithm and its ASIC, and buffer technology for high-acceleration overload
Keywords :
accelerometers; angular velocity measurement; computerised instrumentation; data acquisition; data compression; mechatronics; microsensors; piezoresistive devices; ASIC; MEMS transducer; angle-rate transducer; anisotropic etch; attitude algorithm; buffer technology; control circuit; data compression module; high reliability; high-acceleration overload; high-level integration; micro inertial measurement system; piezoresistor accelerometer; signal acquisition module; single-chip accelerometer; volume production; Computerized monitoring; Hard disks; Humans; Missiles; Quantization; Rockets; Sampling methods; Transducers; Vehicle dynamics; Vehicles;
fLanguage :
English
Journal_Title :
Instrumentation & Measurement Magazine, IEEE
Publisher :
ieee
ISSN :
1094-6969
Type :
jour
DOI :
10.1109/5289.988733
Filename :
988733
Link To Document :
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