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San Andreas Fault Digital Sensor System ‘Phase I’ Assessment

San Andreas Fault Digital Sensor System ‘Phase I’ Assessment. Ric Sanchez Katherine Kendrick Ken Hudnut v. 2 - 4/21/04. N. Courtesy of Ray Weldon. Courtesy of Ray Weldon. Courtesy of Ray Weldon. Digital Sensor System (DSS).

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San Andreas Fault Digital Sensor System ‘Phase I’ Assessment

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

  2. N Courtesy of Ray Weldon

  3. Courtesy of Ray Weldon

  4. Courtesy of Ray Weldon

  5. 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

  6. 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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