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<title>International Telemetering Conference Proceedings, Volume 59 (2024)</title>
<link>http://hdl.handle.net/10150/675363</link>
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<pubDate>Fri, 06 Mar 2026 12:28:39 GMT</pubDate>
<dc:date>2026-03-06T12:28:39Z</dc:date>
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<title>International Telemetering Conference Proceedings, Volume 59 (2024)</title>
<link>http://hdl.handle.net/10150/675451</link>
<description>International Telemetering Conference Proceedings, Volume 59 (2024)
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<pubDate>Tue, 01 Oct 2024 00:00:00 GMT</pubDate>
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<title>Constraints Based Airplane and Data Acquisition System Configuration</title>
<link>http://hdl.handle.net/10150/675449</link>
<description>Constraints Based Airplane and Data Acquisition System Configuration
Rajagopal, Gopinath
Flight Test and Lab Test Data Systems require unique Measurement and Instrumentation configurations before data acquisition. Configuring each acquisition unit individually demands substantial manual effort. Automating this process through software escalates costs due to extensive support needed for diverse hardware and network architectures. To enhance this scenario, a framework has been developed. It uses SHACL constraints as input to dynamically generate forms, APIs, and database schemas in real-time. Leveraging RDF/SHACL—a W3C standard renowned for integrating data based on relationships—the framework dynamically setups for Data Acquisition systems and Aircraft configuration. RDF/SHACL serves as the backbone, facilitating flexibility in configuring various hardware and network architectures while notably reducing manual intervention. Instead of costly software solutions accommodating every hardware or network structure, this approach offers on-the-fly customization without exhaustive software support. By harnessing Semantic web (RDF/SHACL's) standardized data integration capabilities, this framework optimizes configuration for Flight Test and Lab Test Data Systems. It streamlines the process, minimizing manual effort and mitigating the need for extensive software development, ensuring agile and cost-effective setup customization for different acquisition units.
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<pubDate>Tue, 01 Oct 2024 00:00:00 GMT</pubDate>
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<title>Chapter 7 Packet Telemetry: A Retrospective</title>
<link>http://hdl.handle.net/10150/675450</link>
<description>Chapter 7 Packet Telemetry: A Retrospective
Rodittis, Kathy; Kupferschmidt, Ben
The Inter-Range Instrumentation Group’s (IRIG) 106 Chapter 7 standard provides a method for embedding variable length, well-defined data formats within a Chapter 4 Pulse Code Modulation (PCM) stream. Chapter 7’s approach to embedding data streams within a PCM format offers several strengths and weaknesses. This paper will explore the pluses and minuses of the Chapter 7 standard and propose some alternative approaches that have been used successfully.
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<pubDate>Tue, 01 Oct 2024 00:00:00 GMT</pubDate>
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<title>Informing the Simulation: Bridging the Gap Between Model and Reality in Extended Range Artillery</title>
<link>http://hdl.handle.net/10150/675448</link>
<description>Informing the Simulation: Bridging the Gap Between Model and Reality in Extended Range Artillery
Soffer, Avi; Hawkswell, Matthew
For the first time ever the collection of base pressure data, on a projectile with a metal rotating band, has been achieved throughout the interior and intermediate ballistic cycles of a next-generation extended range howitzer. This novel approach utilizes a gyroscopically stabilized Instrumented Ballistic Test Projectile (IBTP) equipped with an On-Board Recorder (OBR). The results offer key insights into the base pressure to breech pressure ratio within next-gen systems. Real-world data is compared to Interior Ballistics of High Velocity Guns (IBHVG2) simulations to identify discrepancies used for improving model accuracy. The collected data, combined with propellant charge dynamics, allows for higher-fidelity structural analyses, conducted with Finite Element Analyses (FEA), and provides a deeper understanding of internal ballistics, paving the way for improved next-generation applications.
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