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TECHNOLOGY DIGEST - Draper Laboratory

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Finally, Figures 14 and 15 show long-term (30-day) SF<br />

and bias stability measured on two SOA-SINS units (S/Ns<br />

028 and 063). The better of the two units demonstrates a<br />

1σ SF stability of 0.73 ppm and a 1σ bias stability of<br />

approximately 2 µg over 30 days.<br />

ppm<br />

µg<br />

12<br />

S/N 028 Avg. SF = 247.4 Hz/g<br />

S/N 063 Avg. SF = 258.8 Hz/g<br />

S/N 028 SF (1σ) = 0.73 ppm<br />

S/N 063 SF (1σ) = 1.22 ppm<br />

Days<br />

Figure 14. Long-term SOA-SINS SF stability.<br />

Figure 15. Long-term SOA-SINS bias stability.<br />

The Silicon Oscillating Accelerometer<br />

SF 063<br />

SF 028<br />

Linear (SF 063)<br />

Linear (SF 028)<br />

2.0<br />

1.5<br />

1.0<br />

0.5<br />

0.0<br />

-0.5<br />

dSF/SF = -0.102 ppm/day<br />

-1.0<br />

-1.5<br />

dSF/SF = -0.011 ppm/day<br />

-2.0<br />

0 5 10 15 20 25 30 35 40<br />

S/N 028 Bias (1σ) = 2.04 µg<br />

S/N 063 Bias (1σ) = 2.68 µg<br />

Days<br />

Bias 063<br />

Bias 028<br />

Linear (Bias 063)<br />

Linear (Bias 028)<br />

5.0<br />

4.0<br />

3.0<br />

2.0<br />

1.0<br />

0.0<br />

-1.0<br />

-2.0<br />

dBias = 0.220 µg/day<br />

-3.0<br />

-4.0<br />

dBias = 0.064 µg/day<br />

-5.0<br />

0 5 10 15 20 25 30 35 40<br />

CONCLUSIONS<br />

<strong>Draper</strong> <strong>Laboratory</strong> is currently developing the SOA, a<br />

MEMS-based inertial-grade sensor. Performance data<br />

acquired to date meet requirements for missile guidance<br />

missions and for high-performance navigation applications<br />

such as the SLBM SINS navigation systems.<br />

The missile and SSBN applications have significantly different<br />

environmental, acceleration dynamic range, and<br />

resolution requirements that are best satisfied by optimizing<br />

the SOA geometry for each application. The design<br />

flexibility and wafer-scale fabrication methods of the silicon<br />

MEMS process enable manufacturing both instrument<br />

designs with essentially zero incremental cost associated<br />

with the additional instrument assembly line. That is, both<br />

versions of the SOA share a common sensor package, electronics<br />

architecture, main housing, and instrument<br />

assembly process.<br />

The MEMS technology is low cost and offers a rapidly<br />

expanding commercial business base to leverage and sustain<br />

accelerometer production and deployment in<br />

next-generation strategic system applications. Integration of<br />

the SOA with mixed-signal, application-specific integrated<br />

circuit (ASIC) electronics offers the promise of a low-cost,<br />

small-size, low-power, and high-reliability strategic-grade<br />

instrument.<br />

REFERENCES<br />

[1] Tang, W., Electrostatic Comb Drive for Resonant Sensor and<br />

Actuator Applications, PhD Dissertation, University of California<br />

at Berkeley, November 21, 1990.<br />

[2] Kourepenis, A., J. Borenstein, J. Connelly, R. Elliott, P. Ward, M.<br />

Weinberg, “Performance of MEMS Inertial Sensors,” 24th Joint<br />

Services Data Exchange for Guidance, Navigation, and Control,<br />

November 16-20, 1998, Anaheim, CA.<br />

[3] Roark and Young, Formulas for Stress and Strain, 5th Edition,<br />

McGraw Hill, 1975.<br />

[4] Nayfeh, Mook, Nonlinear Oscillations, Wiley & Sons, New York,<br />

1979.<br />

[5] Hays, K.M., R.G. Schmidt, W.A. Wilson, J.D. Campbell, D.W.<br />

Heckman, M.P. Gokhale, A Submarine Navigator for the 21st Century, The Boeing Co., IEEE 0-7803-7251-4/02, 2002, pp.<br />

179-188.<br />

[6] Borenstein, J.T., N.D. Gerrish, R. White, M.T. Currie, E.A.<br />

Fitzgerald, “Silicon Germanium Epitaxy: A New Material for<br />

MEMS,” Mat. Res. Soc. Symp., Vol. 657, 2000, pp. 7.4.1.

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