The phenomenology effort was used to define set of
sensor requirements for the airborne demonstration system (Table 1). The
nature of the silicate feature dictated that a sensor was needed that could
spectrally resolve that feature and extend far enough to the longer wavelengths
to obtain data entirely outside the feature. The requirement developed
was to cover the spectral region from 8.3 - 11.0 micrometers with a spectral
resolution greater than 32 wavenumbers. The point spectrometer data, and
in particular the imaging spectrometer data, provided the basis for the
detection algorithm development. These studies suggested that the allowable
sensor noise level (expressed as noise equivalent spectral radiance, NESR)
should be less than 0.01 watts/m2-sr-mm
at 300K. These studies also showed that the mine detection observable was
not always distinct from false alarm sources in the scene, such as certain
mixtures of vegetation and undisturbed soil, but it was found that the
statistical behavior of disturbed sites over emplaced mines was distinct
from backgrounds with similar colors. This statistical phenomenon imposed
a requirement for multiple pixels to be obtained for each mined site. A
minimum number of 30 pixels on target was set to arrive at stable measurements
of variance over mine-like areas.
| Table 1. Phenomenology | Driven Requirements |
| Spectral Range | 8.3-11.0 microns |
| Spectral Resolution | <32 wavenumbers |
| NESR | <0.01 watt/m2-micron-sr |
| Pixels per target | >30 |
In addition to the phenomenology-driven requirements,
the HMD program imposed other requirements on the HMD Demonstration sensor
(Table 2). These programmatic requirements included that the sensor be
airborne and provide real-time detection of mines, that the demonstration
be conducted in a realistic scenario, that the sensor design demonstrated
a clear path to an operational system, and that the sensor be configured
in such a way as to be able to be used as a general LWIR hyperspectral
phenomenology collection platform.
| Table 2. Programmatic Requirements | |
| Airborne | |
| Real-time detection | |
| Realistic demonstration scenario | |
| Path to an operational system | |
| Parallel use as phenomenology
data collection platform |
The AHI (Airborne Hyperspectral Imager) is the demonstration
sensor built in response to the the requirements listed in Tables 1 and
2. AHI is an LWIR pushbroom hyperspectral sensor with gyroscopic image
stabilization and radiance calibration. When configured for mine detection
it is contained in an aerodynamic pod for external mount to a helicopter.
The system also has a configuration for installation on fixed wing aircraft.
The system includes a boresighted digital 3-color CCD linescan camera.
The on-board data collection/ processing system includes a data processor
producing data calibrated to radiance in real-time, and a near-real time
algorithm processor producing mine detections. The on-board storage system
is a RAID disk with 12 Gbyte capacity. The system also includes a ground
data handling, archive and analysis system. Some of the system characteristics
are shown in Table 3.
| Table 3. AHI System Characteristics | |
| Spectral Range | 7-11.5 mm |
| Spectral Resolution
and sampling |
125nm (32
bands)
100nm (256 bands) |
| Angular Resolution | .9 by 2 mrad |
| Swath width | 13 degrees (256 pixels) |
| Sensitivity (NeDT) | <0.1 K |