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Integrating GPS with rotational and inertial sensors Early Warning & DamageMap Kenneth W. Hudnut, Ph.D. Geophysicist USGS, Pasadena Measuring the Rotation Effects of Strong Ground Motion USGS, Pasadena 16 February 2006
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San Andreas fault 35 mm/yr slip rate; >70% of plate motion 1685, 1857 eq’s SoCal is now well ‘wired’ Likely source of most future ‘Big Ones’ Fault physics experiment GPS/INS in near-field ALSM & DG scan ‘net’ Great place to test EEW Build “zipper” arrays Cholame - Simmler Coachella Valley
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GPS network infra- structure forms a foundation for real-time structural damage detection and response Telemetry upgrades Algorithm develop- ment and testing Implementation
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Sensor technology Frequency response position displacement velocity acceleration
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Proper transducers for the EEW job: borehole strain, tilt, strong motion, GPS, gyros? Courtesy of John Langbein (USGS) Gyros Langbein & Bock (2003) GPS Gyros
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GPS/INS (RLG) in airborne imaging: GPS aircraft trajectory relative to ground- based GPS array INS (gyro) for aircraft attitude Laser mirror and/or camera position and orientation very well known New imaging capabilities (also for satellite imagery)
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Sagnac Interferometer RLG’s & FOG’s Designed to sleep for decades then wake up quickly and perform flawlessly for several minutes
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Gyros and MEMS with GPS Stable gyro technology is costly but MEMS-gyro and FOG are lower cost and approaching accuracy Barbour & Schmidt, 1998
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San Andreas - place two bets both ~120 km from Los Angeles (LA) Coachella Valley segment is ~60 km to San Bernardino
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Lone Juniper Ranch and Frazier Park High School Prototype GPS fault slip sensor; up to 10 Hz Spans the San Andreas fault near Gorman, California
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GPS high-rate (1 Hz) analysis Larson, Billich and Choi - see Ji et al. –Sidereal filtering (Larson, Choi) –Stacking (Billich) Significant reduction in long-period drift Compares well now with our static GPS displacements
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Doubly-integrated seismic vs. GPS for Parkfield 2004 (co-located @ PHOB) Raw GPS solution in blue Filtered GPS in green Seismic in red (Boore) These show results prior to final GPS analysis step of stacking, shown previously
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Simplifying assumptions… Sensor technology exists: Inertial BB seismic, accelerometers, gyros GPS - will keep improving Telemetry technology exists
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San Andreas - instrument major lifeline infrastructure crossings
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Courtesy of Erdal Safak (USGS)
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Factor Building at UCLA Prototype for DamageMap PI’s Erdal Safak, Monical Kohler and Paul Davis
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Initial GPS Data from Factor Building Y RMSE = 5 cm X RMSE = 9 cm 100 times better than normal GPS accuracy (SPS now near PPS performance of 6-20 m @ 95% w/ S/A off) Available worldwide $1400/yr.
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Summary Future earthquake monitoring systems will allow faster and better response Tools support rapid and accurate decision-making by emergency responders Fault Slip Sensor and DamageMap concepts Measure fault slip or structural damage directly - don’t need to know anything else - ‘quick & easy’ and simple, robust reliable design obtain more accurate displacement observations, esp. at lifeline fault crossings new instrumentation for dynamic and static displacement address deficiencies due to double-integration of accelerometer records Same R&D effort as for DamageMap instrumentation - now under way with USGS Venture Capital and ANSS start-up funds, but major funding and long-term support for implementation has not yet been identified We are far from being prepared for a Big One in California - it is time to “step it up” - use new technology, fix problems ahead of time
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Ken Hudnut Dept. of the Interior - U. S. Geological Survey 525 South Wilson Ave. Pasadena, CA 91106 626-583-7232 hudnut@usgs.gov
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