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Comment: Automatically updated by Sensor2Confluence-Transporter (aircrafts@ingestsrv1)

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Sensorweb integration
urncamera:macs
contenttypeSummary

The MACS aerial camera is designed to withstand harsh environment like temperatures below -30°C. It has a weight of ~15kg and consists of a computing unit and a sensor head. The sensor head is equipped with matrix array CCD/CMOS/thermal-infrared cameras and is mounted in the fuselage providing free view down. In order to fulfill respective application requirements, sensors, their geometry and spectral ranges are modified. Thus, particular conditions are considered, e.g. flying over brightly reflecting snow, acquisition of highly structured terrain or low flight altitudes without gaps of recorded ground surface. Currently the maximum continuous image acquisition rate is 4 frames per second enabling more than 60% overlap from an altitude of 100 m.

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Sensorweb integration
urncamera:macs
contenttypeMetadata
Manufacturer
Model
Serial No.n/a
Typecamera
SENSOR-Link


Sensorweb integration
urncamera:macs
contenttypeImages

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Sensorweb integration
urncamera:macs
contenttypeContacts
Name Institution Role
Martin GehrmannAlfred Wegener Institute, Helmholtz Centre for Polar and Marine ResearchEngineer In Charge
Daniel SteinhageAlfred Wegener Institute, Helmholtz Centre for Polar and Marine ResearchEditor
Jörg BrauchleDeutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)Data Scientist

Components and Specifications

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