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Comparison of Pumped and Non-Pumped SBE-41CP CTD Sensors on the Slocum
Coastal Electric Glider
Clayton Jones1, Scott Glenn2, John Kerfoot2, Oscar Schofield2, Dave Aragon2, Chip Haldeman2, Dave Pingal11 Teledyne Webb Research Corporation, Falmouth, MA, USA
2 Institute of Marine & Coastal Sciences, Rutgers University, New Brunswick, NJ, USA
Slocum Coastal Electric Glider• Modular
• 3 meters in length
• Uses buoyancy to move through the water column in a saw-tooth pattern
• RF and satellite communications
• Non-pumped SBE-41CP CTD (@ 0.5Hz)• Wide variety of additional payloads
• Dissolved Oxygen• Inherent Optical Properties• Chlorophyll a• Colored Dissolved Organic Matter
Non-Pumped CTD: Cost/Mechanical Considerations
• Lower Power Consumption (~130mW)• Longer Duration Deployments• Requires Less Physical Space• More Space Available for Additional Sensors• Less Expensive
Pumped CTD: Cost/Mechanical Considerations
• Higher Power Consumption (~150mW @ 10mL sec-1)• Shorter Duration• Requires More Physical Space• Less Space Available for Additional Sensors• More Expensive (> 2x un-pumped)
http://www.seabird.com/pdf_documents/datasheets/GliderCTDPrelimSpec3.pdf
Correction of Raw CTD Profiles: Previous Work
• Fofonoff, N. P., S. P. Hayes, and R. C. Millard Jr., 1974: W.H.O.I./Brown CTD microprofiler: Methods of calibration and datahandling. Woods Hole Oceanographic Institution Tech. Rep. WHOI-74-89, 64 pp.
• Lueck, R. G., 1990: Thermal inertia of conductivity cells: Theory. J. Atmos. Oceanic Technol., 7, 741–755.
• Lueck, R. G. and J. L. Picklo, 1990: Thermal inertia of conductivity cells: Observations with a Sea-Bird cell. J. Atmos. Oceanic Technol., 7, 756–768.
• Morison, J., R. Andersen, N. Larson, E. D’Asaro, and T. Boyd, 1994: The correction for thermal-lag effects in Sea-Bird CTD data. J. Atmos. Oceanic Technol., 11, 1151–1164.
• Kerfoot, J.K., Glenn, S., Jones, C., 2006: Correction for Sensor Mis-match and Thermal Lag Effects in Non-Pumped Temperature Conductivity Sensors on the Slocum Coastal Electric Glider. Presented Poster at Ocean Sciences 2006.
• Johnson, G. C., Toole, J.M., Larson, N.G., 2007: Sensor Corrections for Sea-Bird SBE-41CP and SBE-41 CTDs. J. Atmos. Oceanic Technol., 24, 1117-1130.
RU22/RU23 Glider Deployments: September 2009
Non-pumped CTD: RU22 Segment: ru22_2009_264_1_60September 26, 2009 14:42 – September 26, 2009 17:42 GMT
Pumped CTD: RU23 Segment: ru23_2009_264_1_64September 26, 2009 23:22 – September 27, 2009 02:24 GMT
Selected segments were ~4km apart
Correction of Raw CTD Profiles: CT Sensor Mismatch
• Difficult since CT mismatch offsets are much lower than the nominal sampling frequency (0.5 Hz) of the CTD.
Temperature AlignmentComparison of ΔTemp and ΔCond on upcast and downcast – highly variable!
Correction of Raw CTD Profiles: Thermal Inertia
•Theory: Within the same water mass and in the absence of internal wave action, 2 consecutive (upcast and downcast) profiles should possess the same hydrographic (T-S) characteristics.•Select 2 consecutive profiles which do not exhibit internal wave activity. •Morison, et.al (1994):
TT(n) = -bT(n-1) + a[T(n) – T(n-1)]
a = 4fnατ/(1 + 4fnτ) and b = 1 – 2a/α
•Vary α and Τ to minimize the area of the polygon formed by joining the resulting salinity profiles.
Conclusions
• Glider vertical velocity and pitch are key factors in any attempt at correcting un-pumped CTD
• Vertical velocity and pitch vary significantly, depending on ballast accuracy and water column density.
• Pumped CTD provides constant flow which significantly improves success rate of correcting for thermal inertia