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NASA Scientific and Technical Aerospace Reports

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20040071080 <strong>NASA</strong> Stennis Space Center, Bay Saint Louis, MS, USA<br />

Software for Partly Automated Recognition of Targets<br />

Opitz, David; Blundell, Stuart; Bain, William; Morris, Matthew; Carlson, Ian; Mangrich, Mark; Selinsky, T.; Aug. 7, 2002;<br />

2 pp.; In English<br />

Report No.(s): <strong>NASA</strong>/NP-2003-01-00045; SSC-00166; No Copyright; Avail: CASI; A01, Hardcopy<br />

The Feature Analyst is a computer program for assisted (partially automated) recognition of targets in images. This<br />

program was developed to accelerate the processing of high-resolution satellite image data for incorporation into geographic<br />

information systems (GIS). This program creates an advanced user interface that embeds proprietary machine-learning<br />

algorithms in commercial image-processing <strong>and</strong> GIS software. A human analyst provides samples of target features from<br />

multiple sets of data, then the software develops a data-fusion model that automatically extracts the remaining features from<br />

selected sets of data. The program thus leverages the natural ability of humans to recognize objects in complex scenes, without<br />

requiring the user to explain the human visual recognition process by means of lengthy software. Two major subprograms are<br />

the reactive agent <strong>and</strong> the thinking agent. The reactive agent strives to quickly learn the user’s tendencies while the user is<br />

selecting targets <strong>and</strong> to increase the user’s productivity by immediately suggesting the next set of pixels that the user may wish<br />

to select. The thinking agent utilizes all available resources, taking as much time as needed, to produce the most accurate<br />

autonomous feature-extraction model possible.<br />

Author<br />

Computer Programs; Target Recognition; Pattern Recognition<br />

20040071096 <strong>NASA</strong> Stennis Space Center, Bay Saint Louis, MS, USA, Spectral Sciences, Inc., Burlington, MA, USA<br />

Software for Simulation of Hyperspectral Images<br />

Richtsmeier, Steven C.; Singer-Berk, Alex<strong>and</strong>er; Bernstein, Lawrence S.; [2003]; 1 pp.; In English<br />

Report No.(s): <strong>NASA</strong>/NP-2003-09-00039-SSC; SSC-00183; No Copyright; Avail: Other Sources; Abstract Only<br />

A package of software generates simulated hyperspectral images for use in validating algorithms that generate estimates<br />

of Earth-surface spectral reflectance from hyperspectral images acquired by airborne <strong>and</strong> spaceborne instruments. This<br />

software is based on a direct simulation Monte Carlo approach for modeling three-dimensional atmospheric radiative transport<br />

as well as surfaces characterized by spatially inhomogeneous bidirectional reflectance distribution functions. In this approach,<br />

&quot;ground truth&quot; is accurately known through input specification of surface <strong>and</strong> atmospheric properties, <strong>and</strong> it is<br />

practical to consider wide variations of these properties. The software can treat both l<strong>and</strong> <strong>and</strong> ocean surfaces <strong>and</strong> the effects<br />

of finite clouds with surface shadowing. The spectral/spatial data cubes computed by use of this software can serve both as<br />

a substitute for <strong>and</strong> a supplement to field validation data.<br />

Author<br />

Computerized Simulation; Spectral Reflectance; Surface Properties; Meteorological Parameters; Emission Spectra<br />

20040071110 Pennsylvania State Univ., University Park, PA, USA<br />

Optimal Discrete Event Supervisory Control of Aircraft Gas Turbine Engines<br />

Litt, Jonathan, <strong>Technical</strong> Monitor; Ray, Asok; [2004]; 7 pp.; In English<br />

Contract(s)/Grant(s): DAAD19-01-10646; NAG3-2448; NNC04GA49G; No Copyright; Avail: CASI; A02, Hardcopy<br />

This report presents an application of the recently developed theory of optimal Discrete Event Supervisory (DES) control<br />

that is based on a signed real measure of regular languages. The DES control techniques are validated on an aircraft gas turbine<br />

engine simulation test bed. The test bed is implemented on a networked computer system in which two computers operate in<br />

the client-server mode. Several DES controllers have been tested for engine performance <strong>and</strong> reliability.<br />

Author<br />

Optimal Control; Gas Turbine Engines; Control Systems Design; Computer Programs<br />

20040073483 <strong>NASA</strong> Glenn Research Center, Clevel<strong>and</strong>, OH, USA<br />

Development of a Solid-Oxide Fuel Cell/Gas Turbine Hybrid System Model for <strong>Aerospace</strong> Applications<br />

Freeh, Joshua E.; Pratt, Joseph W.; Brouwer, Jacob; May 2004; 16 pp.; In English; Turbo Expo 2004, 14-17 Jun. 2004,<br />

Vienna, Austria<br />

Report No.(s): <strong>NASA</strong>/TM-2004-213054; GT2004-53616; E-14490; No Copyright; Avail: CASI; A03, Hardcopy<br />

Recent interest in fuel cell-gas turbine hybrid applications for the aerospace industry has led to the need for accurate<br />

computer simulation models to aid in system design <strong>and</strong> performance evaluation. To meet this requirement, solid oxide fuel<br />

cell (SOFC) <strong>and</strong> fuel processor models have been developed <strong>and</strong> incorporated into the Numerical Propulsion Systems<br />

194

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