Real-time Data Display for AFTI/F-16 Flight Testing
| Author | : |
| Publisher | : |
| Total Pages | : 22 |
| Release | : 1982 |
| Genre | : |
| ISBN | : |
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Real Time Data Display For Afti F 16 Flight Testing
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Scientific and Technical Aerospace Reports
| Author | : |
| Publisher | : |
| Total Pages | : 1572 |
| Release | : 1992 |
| Genre | : Aeronautics |
| ISBN | : |
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Design Implications from AFTI/F-16 Flight Test
| Author | : |
| Publisher | : |
| Total Pages | : 18 |
| Release | : 1984 |
| Genre | : |
| ISBN | : |
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Proceedings
| Author | : International Telemetering Conference |
| Publisher | : |
| Total Pages | : 950 |
| Release | : 1982 |
| Genre | : Telemeter |
| ISBN | : |
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Real-time Flight Test Analysis and Display Techniques for the X-29A Aircraft
| Author | : |
| Publisher | : |
| Total Pages | : 24 |
| Release | : 1988 |
| Genre | : |
| ISBN | : |
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Proceedings
| Author | : |
| Publisher | : |
| Total Pages | : 680 |
| Release | : 1999 |
| Genre | : Aerospace telemetry |
| ISBN | : |
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NASA SP.
| Author | : |
| Publisher | : |
| Total Pages | : 592 |
| Release | : 1985 |
| Genre | : Aeronautics |
| ISBN | : |
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Aeronautical Engineering
| Author | : |
| Publisher | : |
| Total Pages | : 584 |
| Release | : 1988 |
| Genre | : Aeronautics |
| ISBN | : |
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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
International Aerospace Abstracts
| Author | : |
| Publisher | : |
| Total Pages | : 840 |
| Release | : 1988 |
| Genre | : Aeronautics |
| ISBN | : |
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The Development of an Airborne Instrumentation Computer System for Flight Test
| Author | : |
| Publisher | : |
| Total Pages | : 22 |
| Release | : 1984 |
| Genre | : |
| ISBN | : |
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Instrumentation interfacing frequently requires the linking of intelligent systems together, as well as requiring the link itself to be intelligent. The airborne instrumentation computer system (AICS) was developed to address this requirement. Its small size, approximately 254 by 133 by 140-mm, standard bus, and modular-board configuration give it the ability to solve instrumentation interfacing and computation problems without forcing a redesign of the entire unit. This system has been used on the F-15 aircraft digital electronic engine control (DEEC) and its follow-on engine model derivation (EMD) project, and in an OV-1C Mohawk aircraft stall-speed warning system. The AICS is presently undergoing configuration for use on an F-104 pace aircraft and on the advanced fighter technology integration (AFTI) F-111 aircraft.
