
Design and Simulation of an ARINC-429 Interfacing and Ingestion Module for Real-Time Aircraft Data Acquisition: System Overview and Functional Validation | IJET Volume 12 – Issue 5 | IJET-V12I5P32
IJET
International Journal of Engineering and Techniques
ISSN 2395-1303 · Peer-Reviewed · Open Access
📚 Volume 12, Issue 5
📅 September 29, 2026
📄 Pages 297–301
🔖 ID: IJET-V12I5P32
Table of Contents
ToggleDesign and Simulation of an ARINC-429 Interfacing and Ingestion Module for Real-Time Aircraft Data Acquisition: System Overview and Functional Validation
Author(s)
Chinthala Rupasri, Prof. S. Varadarajan
Abstract
Flight Data Recorders (FDRs) and Cockpit Voice Recorders (CVRs) are the standard systems for capturing aircraft data, designed primarily for post-flight and accident analysis. They do not provide a continuous real-time monitoring channel to the ground. This paper presents the system design and functional simulation of an Interfacing and Ingestion Module (IIM) for the BLUE BOX real-time aircraft telemetry system. The IIM acts as a non-intrusive, parallel monitoring lane alongside the existing FDR/CVR systems. The proposed module accepts flight data, cockpit audio, and cockpit video as inputs and processes them through a chain that includes engineering-unit conversion, CRC-16 error detection, timestamp generation, priority handling, FIFO buffering, and packetization. The system is modelled and simulated in MATLAB/Simulink. Functional validation results covering controlled error injection, CRC-16 error detection, ground-station data recovery, and throughput measurement confirm that the proposed IIM processing chain operates correctly and provides a viable architecture for real-time aircraft data monitoring.
Keywords
BLUE BOX, Interfacing and Ingestion Module (IIM), aircraft data acquisition, real-time monitoring, CRC-16, error detection, MATLAB/Simulink, FDR, CVR, flight data recorder
Conclusion
This paper presented the system-level design and MATLAB/Simulink simulation of the Interfacing and Ingestion Module (IIM) for the BLUE BOX real-time aircraft telemetry system. The IIM provides a non-intrusive, parallel monitoring path alongside existing FDR/CVR recording systems. The implemented processing chain — covering acquisition, engineering-unit conversion, CRC-16 validation, timestamping, priority handling, FIFO buffering, packetization, and ground-station recovery — was validated through four functional simulation tests. CRC-16 error detection was confirmed, ground-station data recovery was demonstrated, and throughput measurement produced a measurable output. These results confirm the functional feasibility of the proposed BLUE BOX IIM architecture and establish a simulation baseline for subsequent hardware development and ARINC-429 protocol-level integration.
References
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[2] R. H. N. S. Jayathissa, ‘Aircraft real time data monitoring,’ Iconic Research and Engineering Journals, vol. 2, no. 8, pp. 37–41, Mar. 2019.
[3] Zhang, Q. Xi, J. Wang, S. Gu, ‘Design of the architecture and algorithm of the civil aviation data real-time analysis system,’ IEEE Access, vol. 12, pp. 66382–66397, 2024.
[4] C. Wang, ‘Application and development of flight data monitoring system in aviation safety management,’ Journal of Computing and Electronic Information Management, vol. 13, no. 1, pp. 10–14, 2024.
[5] U. Özdemir, T. Savas, ‘Development of simulator system to support flight data recording and post flight analysis for trainee pilots,’ Aerospace, vol. 13, no. 2, Art. no. 149, 2026.
[6] B. Natarajan, A. R. Mahasamudram, N. Sharma, ‘A secure, configurable, wireless system for transfer of sensor data from aircraft to ground,’ Defence Science Journal, vol. 72, no. 6, pp. 771–782, 2022.
📋 How to Cite This Paper
Chinthala Rupasri, Prof. S. Varadarajan (2026). Design and Simulation of an ARINC-429 Interfacing and Ingestion Module for Real-Time Aircraft Data Acquisition: System Overview and Functional Validation. International Journal of Engineering and Techniques, 12(5), 297–301. ISSN: 2395-1303. DOI: https://doi.org/10.5281/zenodo.23034435


