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DO-160
DO-160, Environmental Conditions and Test Procedures for Airborne Equipment is a standard for the environmental testing of avionics hardware. It is…
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14 relations
ARP4754
Advisory circular
Avionics
DO-178B
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Papers overview
Semantic Scholar uses AI to extract papers important to this topic.
2019
2019
Measurement and Characterization of Power Lines of Aircraft Flight Test Instrumentation
Ândrei Camponogara
,
T. Oliveira
,
Renato B. Machado
,
Weiler Finamore
,
M. Ribeiro
IEEE Transactions on Aerospace and Electronic…
2019
Corpus ID: 182356474
This paper presents a statistical characterization of power lines used by the flight test instrumentation of a corporate jet as a…
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2018
2018
Prediction of Worst-Case Radiation Immunity in Cable Harnesses
D. Nozadze
,
Yuanzhuo Liu
,
+5 authors
Steve Davidson
IEEE Symposium on Electromagnetic Compatibility…
2018
Corpus ID: 53017638
Radio frequency immunity standards (e.g., RTCA/DO-160G, RTCA/DO-160F) require determining the differential voltage across…
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2018
2018
Measuring Methodology of Conducted Disturbances Generated by Avionic Systems in Aircrafts
W. Sabat
,
D. Klepacki
,
K. Kuryło
,
K. Kamuda
2018
Corpus ID: 67937137
The problems connected with measurements of conducted disturbances emission for on-board devices installed in aircraft have been…
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2017
2017
Three-phase interleaved semi-controlled PFC converter for aircraft application
S. Gangavarapu
,
A. Rathore
IECON - 43rd Annual Conference of the IEEE…
2017
Corpus ID: 12324936
In more electric aircraft (MEA), three phase PFC rectifiers of several kilowatts are required. In this paper, analysis and design…
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2016
2016
Weight reduction of amorphous alloy core electrical transformers for aircraft applications
Wagner Angelo da Silva
,
A. M. Jorge
,
Osmar Ogashawara
International Conference on Electrical Systems…
2016
Corpus ID: 33287742
Catalogues of manufactured transformers show that amorphous alloy core transformers applied to 50 or 60 Hz lines have about 70…
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2016
2016
Aircraft Engine Control Unit (FADEC) Design Assessment for Dynamic Analysis
J. Preethi
,
Dr. B. M. Nandeeshaiah
2016
Corpus ID: 212547893
The FADEC's basic purpose is to provide optimum engine efficiency for a g iven flight condition. Hence p resent study focuses o n…
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2014
2014
Saturation harmonic effect of induction motor on aircraft power quality
Xiaofei Du
,
Chu Sun
,
Longsheng Guo
,
Y. Zhou
9th IEEE Conference on Industrial Electronics and…
2014
Corpus ID: 15282958
Aero variable-frequency generators are employed in current airplanes to provide high power for increasing loads. Due to nonlinear…
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2014
2014
Energy harvesting for aerospace: Application possibilities
L. Janák
,
Vladislav Singule
Proceedings of the 16th International Conference…
2014
Corpus ID: 28813019
This paper deals with the state of art in the field of energy harvesting systems. The paper mainly aims to the novel field of…
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2013
2013
Input and output EMI filter design procedure for matrix converters
Q. Wang
,
B. Wen
,
X. Zhang
,
R. Burgos
,
P. Mattavelli
,
D. Boroyevich
IECON - 39th Annual Conference of the IEEE…
2013
Corpus ID: 19337810
This paper proposes a detailed step-by-step design procedure for the input and output EMI filter of a matrix converter (MC…
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2006
2006
PDN Design Strategies : I . Ceramic SMT Decoupling Capacitors – What Values Should I Choose ?
R. Olsen
,
J. Knighten
,
+4 authors
J. Drewniak
2006
Corpus ID: 14719527
Emissions in aircraft communication and navigation bands are measured for the latest generation of wireless phones. The two…
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