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APPLICATIONS FOR A PORTABLE PC/104 BASED INSTRUMENTATION CONTROLLERSchumacher, Gary A. 10 1900 (has links)
International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and Convention Center, San Diego, California / PC based instrumentation and telemetry processing systems are attractive because of their
ease of use, familiarity, and affordability. The evolution of PC computing power has
resulted in a telemetry processing system easily up to most tasks, even for control of and
processing of data from a very complex system such as the Common Airborne
Instrumentation System (CAIS) used on the new Lockheed-Martin F-22. A complete
system including decommutators, bit synchronizers, IRIG time code readers, simulators,
DACs, live video, and tape units for logging can be installed in a rackmount, desktop, or
even portable enclosure.
The PC/104 standard represents another step forward in the PC industry evolution towards
the goals of lower power consumption, smaller size, and greater capacity. The advent of
this standard and the availability of processors and peripherals in this form factor has made
possible the development of a new generation of portable low cost test equipment.
This paper will outline the advantages and applications offered by a full-function, standalone,
rugged, and portable instrumentation controller. Applications of this small (5.25"H x
8.0"W x 9.5"L) unit could include: flight line instrumentation check-out, onboard aircraft
data monitoring, automotive testing, small craft testing, helicopter testing, and just about
any other application where small-size, affordability, and capability are required.
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DETERMINATION OF AN OPTIMAL DATA BUS ARCHITECTURE FOR A FLIGHT DATA SYSTEMCrawford, Kevin, Johnson, Martin 10 1900 (has links)
International Telemetering Conference Proceedings / October 22-25, 2001 / Riviera Hotel and Convention Center, Las Vegas, Nevada / NASA/Marshall Space Flight Center (MSFC) is continually looking for methods to reduce cost
and schedule while keeping the quality of work high. MSFC is NASA’s lead center for space
transportation and microgravity research. When supporting NASA’s programs several decisions
concerning the avionics system must be made. Usually many trade studies must be conducted to
determine the best ways to meet the customer’s requirements. When deciding the flight data
system, one of the first trade studies normally conducted is the determination of the data bus
architecture. The schedule, cost, reliability, and environments are some of the factors that are
reviewed in the determination of the data bus architecture. Based on the studies, the data bus
architecture could result in a proprietary data bus or a commercial data bus. The cost factor
usually removes the proprietary data bus from consideration. The commercial data bus
architecture’s range from Versa Module Euro card (VME) to Compact PCI to STD 32 to PC 104.
If cost, schedule and size are prime factors, VME is usually not considered. If the prime factors
are cost, schedule, and size then Compact PCI, STD 32 and PC 104 are the choices for the data bus
architecture.
MSFC’s center director has funded a study from his discretionary fund to determine an optimal
low cost commercial data bus architecture. The goal of the study is to functionally and
environmentally test Compact PCI, STD 32 and PC 104 data bus architectures. This paper will
summarize the results of the data bus architecture study.
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Development of a Sag Monitoring Instrument based on an Embedded System PlatformGaikwad, Anish Madhukar 11 May 2002 (has links)
Small size, low weight and rugged environmental specifications characterize embedded systems. PC/104 is an embedded system architecture that implements the compact version of the PC (ISA and PCI) buses. The PC/104 architecture uses 104 pins for stacking different boards and eliminates the need for card edges and backplanes. Standardizing hardware and software around PC architecture substantially reduces the development cost, time and risks involved. The purpose of this study is to develop an environmentally rugged and portable instrument based on the PC/104 architecture for measuring and recording voltage sags as per the International Electrotechnical Commission (IEC) standards 61000-4-30 and 61000-2-8. Two different central processing units (CPU) for the instrument are evaluated in terms of hardware setup, cost and performance. The overall performance of the instrument using either CPU indicates that the instrument can be reliably used to measure voltage sags.
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Návrh a realizace aircraft interface device / Design and realization of aircraft interface deviceJankech, Tomáš January 2015 (has links)
The aim of this master’s thesis is a design and a realization of an interface device for various aircraft buses. The work shows the issue of Aircraft Interface Device and describes the most used types of avionics buses. It deals with the theoretical design of the PCI/104–Express module and is using modularity for maximum configurability of the device. The work also brings the selection of appropriate components and their use in design. The last part describes a firmware architecture.
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COMMON AIRBORNE INSTRUMENTATION SYSTEM; A FRESH LOOKGrace, Thomas 10 1900 (has links)
International Telemetering Conference Proceedings / October 22-25, 2001 / Riviera Hotel and Convention Center, Las Vegas, Nevada / The US Government originally funded the development of the Common Airborne Instrumentation
System (CAIS) to address industry-wide compatibility, maintenance, and commonality issues. Although
initially targeted for US Department of Defense (DoD) programs, CAIS is also being used throughout
the world in many commercial applications. This paper provides a fresh look at the evolution of the
CAIS concept starting with some historical background of the CAIS Program, an overview of the CAIS
System Architecture and recent trends in the use of “Commercial Off The Shelf (COTS)” products and
technology.
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Analysis of hardware requirements for airborne tactical mesh networking nodes / An analysis of tactical mesh networking hardware requirements for airborne mobile nodesMilicic, Gregory J. 03 1900 (has links)
Approved for public release, distribution is unlimited / Wireless mesh mobile ad hoc networks (MANETs) provide the military with the opportunity to spread information superiority to the tactical battlespace in support of network-centric warfare (NCW). These mesh networks provide the tactical networking framework for providing improved situational awareness through ubiquitous sharing of information including remote sensor and targeting data. The Naval Postgraduate School's Tactical Network Topology (TNT) project sponsored by US Special Operations Command seeks to adapt commercial off the shelf (COTS) information technology for use in military operational environments. These TNT experiments rely on a variety of airborne nodes including tethered balloon and UAVs such as the Tern to provide reachback from nodes on the ground to the Tactical Operations Center (TOC) as well as to simulate the information and traffic streams expected from UAVs conducting surveillance missions and fixed persistent sensor nodes. Airborne mesh nodes have unique requirements that can be implemented with COTS technology including single board computers and compact flash. / Lieutenant, United States Navy
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