A MISSILE INSTRUMENTATION SYSTEM DESIGN APPROACH
dc.contributor.author | Davis, Chuck | |
dc.contributor.author | Penharlow, David | |
dc.date.accessioned | 2016-05-27T22:59:39Z | |
dc.date.available | 2016-05-27T22:59:39Z | |
dc.date.issued | 1984-10 | |
dc.identifier.issn | 0884-5123 | |
dc.identifier.issn | 0074-9079 | |
dc.identifier.uri | http://hdl.handle.net/10150/611017 | |
dc.description | International Telemetering Conference Proceedings / October 22-25, 1984 / Riviera Hotel, Las Vegas, Nevada | en_US |
dc.description.abstract | Requirements and design constraints of a missile instrumentation system are identified. These considerations were applied and a programmable master/slave PCM encoder with integral signal conditioning was selected for a major classified missile program. The engineering philosophy and hardware selected for this application are presented in this paper. | |
dc.description.sponsorship | International Foundation for Telemetering | en |
dc.language.iso | en_US | en |
dc.publisher | International Foundation for Telemetering | en |
dc.relation.url | http://www.telemetry.org/ | en |
dc.rights | Copyright © International Foundation for Telemetering | en |
dc.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | |
dc.title | A MISSILE INSTRUMENTATION SYSTEM DESIGN APPROACH | en_US |
dc.type | text | en |
dc.type | Proceedings | en |
dc.contributor.department | General Dynamics Convair Division | en |
dc.contributor.department | Aydin Vector Division | en |
dc.identifier.journal | International Telemetering Conference Proceedings | en |
dc.description.collectioninformation | Proceedings 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.dateFOA | 2018-06-22T23:11:08Z | |
html.description.abstract | Requirements and design constraints of a missile instrumentation system are identified. These considerations were applied and a programmable master/slave PCM encoder with integral signal conditioning was selected for a major classified missile program. The engineering philosophy and hardware selected for this application are presented in this paper. |