1. 4K by 4K monochrome quality aerial imagery
2. Fully oriented 4K by 4K aerial imagery
3. Improve the geometrical and spectral resolution
of the image sensor (multi- and hyperspectral
systems), extend onboard sensor capabilities with
laser ranging and/or profiling, IFSAR, etc.,
technologies
4. Oriented 4K by 4K aerial imagery with DEM
S. Data described above with automatically
extracted features
6. Increase real-time airborne processing power,
integrate imaging into the GPS/INS positioning
system, introduce for target recognition/tracking.
The basic objectives of AIMS™ phases 1 and 2, have
been accomplished by now. Based on the validated
performance of the positioning component, preparations
are underway to fly the AIMS™ prototype with
different imaging sensors.
FETT
Figure 5. Callahan, FL, DEM test site.
Test flights 12 and 13 were already planned to
accommodate a laser scanner in a future flight. The
objective is to deliver high-precision DEM over
transportation structures. A typical image from the
project area is shown in Figure S
Figure 6. GPS points, NASA Stennis Space Center, MS.
Preparations are also well underway to fly a multi- and
hyperspectral sensor system with cooperation of NASA
Stennis Space Center. As of the writing of this paper,
sensor calibration is being carried out to establish the
boresighting of the different sensors relative to the
AIMS™ positioning components. Figure 6 depicts the
GPS reference points spreading over the Stennis Space
Center facilities. Once sensor calibration is done,
reference agricultural test sites will be flown.
6. CONCLUSION
This paper reviews the Airborne Integrated Mapping
System (AIMS™) being developed by the Center for
Mapping. The discussion introduces the overall system
architecture and the imaging component. The prototype
system has shown good calibration performance over a
large number of test flights. Current efforts are focused
on the integration of complimentary imaging sensors
including laser scanner and a multi- and hyperspectral
image acquisition system.
ACKNOWLEDGEMENTS
This work was supported by the NASA Stennis Space
Center, MS, Commercial Remote Sensing Program
grant #NAG13-42, and a grant from Litton Systems,
Inc.
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