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dc.contributor.authorEccles, Lee H.
dc.contributor.authorMalchodi, Lawrence A.
dc.date.accessioned2016-06-14T15:23:01Z
dc.date.available2016-06-14T15:23:01Z
dc.date.issued1991-11
dc.identifier.issn0884-5123
dc.identifier.issn0074-9079
dc.identifier.urihttp://hdl.handle.net/10150/613056
dc.descriptionInternational Telemetering Conference Proceedings / November 04-07, 1991 / Riviera Hotel and Convention Center, Las Vegas, Nevadaen_US
dc.description.abstractThe Boeing Commercial Airplane Group’s Flight Test Engineering organization is developing two new data acquisition systems. One of these systems will be used to investigate problems on aircraft which are being flown by the airlines in normal airline service. The second system is intended for use as the data acquisition system during the certification of the new 777 airplane. The two systems will differ in physical size, capacity and the recorder being used. They are expected to use as much of the same hardware and software as possible. This paper discusses the design of both systems.
dc.description.sponsorshipInternational Foundation for Telemeteringen
dc.language.isoen_USen
dc.publisherInternational Foundation for Telemeteringen
dc.relation.urlhttp://www.telemetry.org/en
dc.rightsCopyright © International Foundation for Telemeteringen
dc.titleNEW BOEING FLIGHT TEST DATA ACQUISITION SYSTEMSen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentBoeing Commercial Airplane Groupen
dc.identifier.journalInternational Telemetering Conference Proceedingsen
dc.description.collectioninformationProceedings from the International Telemetering Conference are made available by the International Foundation for Telemetering and the University of Arizona Libraries. Visit http://www.telemetry.org/index.php/contact-us if you have questions about items in this collection.en
refterms.dateFOA2018-09-11T12:53:09Z
html.description.abstractThe Boeing Commercial Airplane Group’s Flight Test Engineering organization is developing two new data acquisition systems. One of these systems will be used to investigate problems on aircraft which are being flown by the airlines in normal airline service. The second system is intended for use as the data acquisition system during the certification of the new 777 airplane. The two systems will differ in physical size, capacity and the recorder being used. They are expected to use as much of the same hardware and software as possible. This paper discusses the design of both systems.


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