SQM-5002 SATELLITE QUALITY MONITOR | ||||||||||
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Overview
The Model SQM-5002 Satellite Quality Monitor is a computer-controlled, diffuse light source for field-calibrating narrow band filter radiometers and CCD imagers in-situ. A commercialization of the SeaWIFS Quality Monitor initially developed by NASA’s Goddard Space Flight Center and NIST, the SQM-5002 supports field stability checks of ground-level filter radiometers to assist with verifying the performance of remote sensing platforms. While the lamp housing and components are nearly identical to the original NASA design, the control system and power supply were re-designed to enhance performance and are enclosed in a watertight steel NEMA-4X enclosure. The SQM-5002 is a complete system and provides three optical output intensity levels. It can be readily adapted to a wide variety of optical detectors both in the laboratory and in the field. Principle of Operation The SQM-5002 is a computer-controlled stabilized light source and can be run stand alone or monitored by a software application. An internal thermally stabilized current regulation circuit ensures precise current regulation to two independent lamp rings, providing low, medium or high power output. Shunt temperatures as well as the lamp housing temperatures are monitored during operation. When operated independently, these lamps result in three possible optical power levels. Two filter-detector channels and a third unfiltered detector are positioned within the lamp housing to permit direct optical monitoring of the lamp rings and the integrating cavity itself. These three detectors are thermally stabilized via a thermoelectrically-cooled mechanical housing to approximately 35° C, and their outputs are continuously monitored during system operation. An exit aperture provides spectrally and spatially uniform light flux to the device under test (DUT). Mechanical alignment fixtures are available for a variety of filter radiometers.
Features
Applications The SQM-5002 is a cost-effective field calibration source that is well suited to many applications:
Software Control The system is operated and monitored via a GUI built with Lab-ViewÔ . It runs on a either a Windows PC or Macintosh and can operate simultaneously with other software such as radiometer control applications. All system settings and performance logging is controlled by software, including lamp power, cooling fan and pre-heater. It provides continuous independent verification of optical output through 3 thermally-stabilized internal optical detectors. Instrument Specifications NASA Goddard personnel conducted optical performance tests on a production unit built under contract; for detailed specifications a comprehensive discussion on the system design can be found in these peer-reviewed papers:
Specifications
Sensor Mount The device under test is mechanically interfaced to the lamp housing via an included kinematic mount. A universal optics table option is recommended to accommodate a wide variety or radiometers. Reusable Flight Case A reusable flight case option is recommended to protect your system.
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