Design and Implementation of PCM/FM Telemetry Systems for Aircraft and Missile Testing During Flight Test Procedure | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 35, Volume 14, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011, May 2011, Page 1-15 PDF (561.7 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.2011.23257 | ||||
 View on SCiNiTO | ||||
| Authors | ||||
| Z. Filipovic1; G. Dikic2 | ||||
| 1Institute Gosa, Belgrade, Serbia. | ||||
| 2Military Academy, Belgrade, Serbia. | ||||
| Abstract | ||||
| This paper describes the overall system design and performance characteristics of a complete PCM/FM telemetry system for aircraft and missile testing during flight test procedure. The system encompasses subsystems for airborne data acquisition and flight line check-out, a compatible ground telemetry system. The airborne part includes a variety of component for measurement all relevant aircraft parameters. The ground telemetry system receive signal from flying object, performs real time data processing, test control and a data processing system for post flight analysis. The system represents a fully integrated approach to flight test systems which addresses the end-to-end requirements from airborne data acquisition and real time flight monitoring through aircraft performance and stability/control analysis. | ||||
| Keywords | ||||
| PCM/FM telemetry system; Data acquisition; real time acquisition; airborne subsystem; ground station; post flight analyses | ||||
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