Attention:
Please note that operation of the AISA Eagle hyperspectral camera requires experienced scientific staff on board the aircraft.
Summary
Contacts
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.
| Name | Model | Type |
|---|---|---|
| Fibre-optics downwelling irradiance sensor | FODIS | Radiation Meter |
| Inertial and GPS Navigation System | RT3000 | inertial measurement unit |
Specifications of AISA Eagle (without mounting)
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)
Dimension (W x D x H) |
120 x 71 x 184 mm |
|---|---|
Weight |
1.4 kg |
Power Supply |
10-50 VDC |
Position
Data logging, storage and archiving
Logged parameter
Rawdata storage on board
During flight AISA Eagle data are stored on the operator PC.
Data archiving on land
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.