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                       FIGURE 19.28  A typical signal conditioning arrangement for single chip microaccelerometers.
                       Piezoresistive Transducers
                       Piezoresistive transducers generally have high-amplitude outputs, low-output impedance, and low intrin-
                       sic noise. Most of these transducers are designed for constant-voltage excitations. They are usually
                       calibrated for constant-current excitations to avoid external interference. Many piezoresistive transducers
                       are configured as full-bridge devices. Some have four active piezoresistive arms, together with two fixed
                       precision resistors to permit shunt calibration.
                       Microaccelerometers
                       In microaccelerometers signal-conditioning circuitry is integrated within the same chip as the sensor. A
                       typical example of the signal-conditioning circuitry is given in Fig. 19.28 in block diagram form. In this
                       type of accelerometer, the electronic system is essentially a crystal-controlled oscillator circuit and the
                       output signal of the oscillator is a frequency-modulated acceleration signal. Some circuits provide a
                       buffered square-wave output that can be directly interfaced digitally. In these cases the need for analog-
                       to-digital (A/D) conversion is eliminated, thus removing one of the major sources of errors. In other
                       types of accelerometers, signal conditioning circuits such as A/D converters are retained within the chip.
                       Force Feedback Accelerometers
                       Signals from force feedback accelerometers often must be digitized for use in digital systems. A common
                       solution is to use voltage to frequency or current to frequency converters to convert the analog signals
                       to train pulses. These converters are expensive, often as much as the accelerometer, and add as much to
                       the error budget.
                         Here, it is worth mentioning that GPS systems are becoming add-ons to many position sensing
                       mechanisms. Because of antenna dynamics, shadowing, multipath effects, and to provide redundancy
                       for critical systems such as aircraft, many of these systems require inertial aiding, tied-in with accelerom-
                       eters and gyros. With the development of micromachining, small and cost-effective GPS assisted inertial
                       systems will be available in the near future. These developments will require extensive signal processing
                       with a high degree of accuracy. Dynamic ranges on the order of a million to one (e.g., 30–32 bits) need
                       to be dealt with. In order to achieve accuracy requirements, a great challenge awaits the signal processing
                       practitioner.

                       References

                        1. Bentley, J. P., Principles of Measurement Systems, 2nd ed., Burnt Mill, UK: Longman Scientific and
                          Technical, 1988.
                        2. Doebelin, E. O., Measurement Systems: Application and Design, 4th ed., Singapore: McGraw-Hill, 1990.
                        3. Frank, R., Understanding Smart Sensors, Boston: Artech House, 1996.
                        4. Harris, C., Shock and Vibration Handbook, 4th ed., McGraw-Hill, 1995.
                        5. Holman, J. P., Experimental Methods for Engineers, 5th ed., Singapore: McGraw-Hill, 1989.


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