Avionics data buses: an overview

Zhang, J.-G.; Pervez, Anjum; Sharma, A.

doi:10.1109/maes.2003.1183865

Cited by 9 publications

(3 citation statements)

References 12 publications

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“…device by transformer coupling connection. UMA-2000 interface with 1553 bus were accomplished with a developed cable with a pre-studied design for adaptation between the output interface of the 1553 bus and UMA-2000 as shown in the following figure (5).…”

Section: Methodsmentioning

confidence: 99%

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Implementation of Acquisition Data Recorder for an Aircraft

Shawky

Ezzat

Azouz

et al. 2010

The International Conference on Electrical Engineering

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Capturing and retrieving data from aircraft (A/C) for the sake of flight test recording, maintenance and crash recording or mission recording& analysis are crucial for fault diagnoses and pilots training. Acquired data from A/C are sorted into two categories; first one is analog/discrete data from analog systems, while the second concerns the MIL-STD 1553 serial data of all its connected remote terminals. UMA2000 is a stateof-art Flight Data Recorder (FDR) was used as a programmable Data Acquisition System for acquiring analog, digital signals and MIL-STD 1553 data acquisition channels, as a Bus Monitor to gather information of flight mission from several systems on the A/C. This paper introduces a way of interfacing UMA2000 on the aircraft platform, gathering, decompressing, decoding, analyzing and converting data to engineering units for retrieving the mission information about the status of the engine, avionics, mission computers ….etc.

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Section: Methodsmentioning

confidence: 99%

“…This reflected wave will then be coupled back into the original wave on the main bus. The portion of the wave that traveled down the stub and back will introduce a time delay that creates a phase distortion in the transmitted waveform [5].…”

Section: Figure (1): Mil-std-1553 Transmit Data Pathmentioning

confidence: 99%

Implementation of Acquisition Data Recorder for an Aircraft

Shawky

Ezzat

Azouz

et al. 2010

The International Conference on Electrical Engineering

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“…From this moment, several military data buses have been developed; i.e. MIL-STD-1773, STANG 3910 or High Speed Data Bus (HSDB) [2].…”

Section: Introductionmentioning

confidence: 99%

Design and performance of an adaptation middleware interface for a civil avionic bus

Parrilla

Rodrı́guez

Simón-Muela

et al. 2009

2009 IEEE/AIAA 28th Digital Avionics Systems Conference

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The main motivation of this work is the study, design and implementation of a Middleware software layer to manage the data exchange in current avionics data buses. Thus, this layer is based on an objectoriented structure using several software design patterns like Abstract Factory, Factory Method and Singleton. The most important benefit of this new software tool is that simplifies, makes faster and more robust real-time communications in present avionics data buses. In addition, this layer provides higher design flexibility in distributed communication systems obtaining more reusable and portable software interfaces. What's more, this Middleware software tool makes independent a specific avionics application from each other in the data bus. In consequence and thanks to the new implemented tool, there is no need of ad-hoc communication software, developed by the hardware manufacturer, for each avionics embedded card in the data bus.

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