Issue 10 Volume 41 May 16, 2003
Issue 10 Volume 41 May 16, 2003
Issue 10 Volume 41 May 16, 2003
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<strong>2003</strong>0033048 NASA Kennedy Space Center, Cocoa Beach, FL, USA<br />
Advanced Data Acquisition Systems<br />
Perotti, J.; [<strong>2003</strong>]; 5 pp.; In English; Propulsion Measurement Sensor Development Workshop, 13-15 <strong>May</strong> <strong>2003</strong>, Huntsville,<br />
AL, USA; Original contains black and white illustrations<br />
Report No.(s): KSC-<strong>2003</strong>-049; No Copyright; Avail: CASI; A01, Hardcopy<br />
Current and future requirements of the aerospace sensors and transducers field make it necessary for the design and<br />
development of new data acquisition devices and instrumentation systems. New designs are sought to incorporate self-health,<br />
self-calibrating, self-repair capabilities, allowing greater measurement reliability and extended calibration cycles. With the<br />
addition of power management schemes, state-of-the-art data acquisition systems allow data to be processed and presented to<br />
the users with increased efficiency and accuracy. The design architecture presented in this paper displays an innovative<br />
approach to data acquisition systems. The design incorporates: electronic health self-check, device/system self-calibration,<br />
electronics and function self-repair, failure detection and prediction, and power management (reduced power consumption).<br />
These requirements are driven by the aerospace industry need to reduce operations and maintenance costs, to accelerate<br />
processing time and to provide reliable hardware with minimum costs. The project’s design architecture incorporates some<br />
commercially available components identified during the market research investigation like: Field Programmable Gate Arrays<br />
(FPGA) Programmable Analog Integrated Circuits (PAC IC) and Field Programmable Analog Arrays (FPAA); Digital Signal<br />
Processing (DSP) electronic/system control and investigation of specific characteristics found in technologies like: Electronic<br />
Component Mean Time Between Failure (MTBF); and Radiation Hardened Component Availability. There are three main<br />
sections discussed in the design architecture presented in this document. They are the following: (a) Analog Signal Module<br />
Section, (b) Digital Signal/Control Module Section and (c) Power Management Module Section. These sections are discussed<br />
in detail in the following pages. This approach to data acquisition systems has resulted in the assignment of patent rights to<br />
Kennedy Space Center under U.S. patent # 6,462,684. Furthermore, NASA KSC commercialization office has issued licensing<br />
rights to Circuit Avenue Netrepreneurs, LLC , a minority-owned business founded in 1999 located in Camden, NJ.<br />
Derived from text<br />
Systems Health Monitoring; Smart Structures; Data Acquisition; Architecture (Computers); Maintenance; Fault Detection;<br />
Calibrating<br />
61<br />
COMPUTER PROGRAMMING AND SOFTWARE<br />
Includes software engineering, computer programs, routines, algorithms, and specific applications, e.g., CAD/CAM. For computer<br />
software applied to specific applications, see also the associated category.<br />
<strong>2003</strong>0032283 NASA Ames Research Center, Moffett Field, CA, USA<br />
Using Grid Benchmarks for Dynamic Scheduling of Grid Applications<br />
Frumkin, Michael; Hood, Robert; [<strong>2003</strong>]; 11 pp.; In English; HPDC12, 22-24 Jun. <strong>2003</strong>, Seattle, WA, USA; Original contains<br />
black and white illustrations<br />
Contract(s)/Grant(s): 704-42-42; Copyright; Avail: CASI; A03, Hardcopy<br />
Navigation or dynamic scheduling of applications on computational grids can be improved through the use of an<br />
application-specific characterization of grid resources. Current grid information systems provide a description of the resources,<br />
but do not contain any application-specific information. We define a GridScape as dynamic state of the grid resources. We<br />
measure the dynamic performance of these resources using the grid benchmarks. Then we use the GridScape for automatic<br />
assignment of the tasks of a grid application to grid resources. The scalability of the system is achieved by limiting the<br />
navigation overhead to a few percent of the application resource requirements. Our task submission and assignment protocol<br />
guarantees that the navigation system does not cause grid congestion. On a synthetic data mining application we demonstrate<br />
that Gridscape-based task assignment reduces the application tunaround time.<br />
Author<br />
Computational Grids; Architecture (Computers); Automatic Control; Programming (Scheduling); Computer Systems<br />
Programs; Machine Learning<br />
<strong>2003</strong>0032435 NASA Ames Research Center, Moffett Field, CA, USA<br />
Characterization of Model-Based Reasoning Strategies for Use in IVHM Architectures<br />
Poll, Scott; Iverson, David; Patterson-Hine, Ann; [<strong>2003</strong>]; 13 pp.; In English; Original contains black and white illustrations;<br />
No Copyright; Avail: CASI; A03, Hardcopy<br />
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