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San Andreas Fault Digital Sensor System ‘Phase I’ Assessment Ric Sanchez Katherine Kendrick Ken Hudnut v. 2 - 4/21/04.

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Presentation on theme: "San Andreas Fault Digital Sensor System ‘Phase I’ Assessment Ric Sanchez Katherine Kendrick Ken Hudnut v. 2 - 4/21/04."— Presentation transcript:

1 San Andreas Fault Digital Sensor System ‘Phase I’ Assessment Ric Sanchez Katherine Kendrick Ken Hudnut v. 2 - 4/21/04

2 N Courtesy of Ray Weldon

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6 Digital Sensor System (DSS) The first complete turn-key all- digital medium format mapping system with: Built in Flight Management System Integrated POS AV Direct Georeferencing System True Colour and CIR Digital Imager Ruggedized data logger and pressurized drive Courtesy of Applanix-Emerge

7 DSS Specifications Array size 4092 X 4077 pixels, 9 micron pixel size Lenses Standard: 55mm, 37 deg FOV, True Color and CIR Optional: 35mm, 55.4 deg FOV, True Color only Shutter Speed 1/125 - 1/4000 sec Imaging time 4 sec GSD 0.05 to 1 meter (lens and platform dependent) Smear < 10% typical Housing Ruggedized exoskeleton with lens stabilization Positioning 0.05 - 0.3 meter, post mission Attitude 0.008 - 0.15 deg, post mission FMS TrackAir EZtrack or external third-party unit Data Logging 80GB removable hard drive and pressurized Data Brick Courtesy of Applanix-Emerge

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