The University of Arizona Campus Repository > Conference Proceedings > International Telemetering Conference > International Telemetering Conference Proceedings, Volume 20 (1984) >
A MISSILE INSTRUMENTATION SYSTEM DESIGN APPROACH
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- 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.
- International Foundation for Telemetering
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Full metadata record
|dc.title||A MISSILE INSTRUMENTATION SYSTEM DESIGN APPROACH||en_US|
|dc.contributor.department||General Dynamics Convair Division||en|
|dc.contributor.department||Aydin Vector Division||en|
|dc.rights||Copyright © International Foundation for Telemetering||en|
|dc.publisher||International Foundation for Telemetering||en|
|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.||en|
|dc.description.sponsorship||International Foundation for Telemetering||en|
|dc.identifier.journal||International Telemetering Conference Proceedings||en|
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