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Please note that operation of the AISA Eagle hyperspectral camera requires experienced scientific staff on board the aircraft. |
Summary
| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | Summary |
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AISA Eagle is a system for VNIR hyperspectral imaging. It acquires full, high quality hyperspectral data with 1000 swath pixels and high image rates. AISA Eagle is a complete, pushbroom system that consists of a compact hyperspectral sensor head, GPS/INS sensor, and data acquisition unit in a rugged PC. An additional Fiber-Optic Downwelling Irradiance Sensor (FODIS) simultaneously aquires data of incoming radiation. Sensor-Info: aircraft:bt-67:aisa_100028, 6992 |
| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | Metadata |
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| Manufacturer | Spectral Imaging Ltd. (Specim Ltd.) |
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| Model | AISA Eagle |
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| Serial No. | 100028 |
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| Type | Spectrometer |
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| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | Images |
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| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | Contacts |
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| Name | Institution | Role |
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| Gerit Birnbaum | Alfred-Wegener-Institut | Device Contact |
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Components and Specifications
The AISA Eagle system consists of the hyperspectral camera itself, a GPS / INS unit , an irradiance sensor, an operator PC and a power distribution box.
| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | Subdevices |
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| Name | Model | Serial Number |
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| Fibre-optics downwelling irradiance sensor | FODIS | n/a | | Inertial and GPS Navigation System | RT3000 | 230 |
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Specifications of AISA Eagle (without mounting)
| Metadata list |
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|| Dimension (W x D x H)| 146 x 146 x 350 mm||
|| Weight | 7 kg||
|| Power Supply | 28 VDC ||
|| Data interface | Ethernet || |
Specifications of GPS/INS RT3100 (without mounting)
| Metadata list |
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|| Dimension (W x D x H)| 120 x 71 x 184 mm ||
|| Weight | 1.4 kg ||
|| Power Supply | 10-50 VDC ||
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Position
| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | LocalFrame |
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| The specral sensor and the attached GPS INS unit are installed on an opening in the underfloor compartment. Power box and operator PC are mounted on the cabin floor. The FODIS sensor is attached to the cabin roof. |
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Data logging, storage and archiving
Logged parameter
| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | Parameters |
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| Parameter | Sensor Output Type | Unit |
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| Spectral radiance | spectral radiance | Wm-2 sr-1 um-1 | | irradiance | irradiance | W/m^2 | | roll | attitude | degree | | pitch | attitude | degree | | yaw | attitude | degree | | latitude | latitude | decimal degrees | | longitude | longitude | decimal degrees |
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Rawdata storage on board
| Metadata (Metadata Plugin) |
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During flight AISA Eagle data are stored on the operator PC. |
Data archiving on land
| Metadata (Metadata Plugin) |
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After the flight AISA Eagle data have to be downloaded and are stored within the external devices file system of the aircraft data managment system (DMS). Additionally, raw data of the GPS/INS unit can be downloaded. |
Documentation
| Sensorweb integration |
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| urn | aircraft:bt-67:aisa_100028 |
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| contenttype | Resources |
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