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BS IEC 62396-3:2013

$142.49

Process management for avionics. Atmospheric radiation effects – System design optimization to accommodate the single event effects (SEE) of atmospheric radiation

Published By Publication Date Number of Pages
BSI 2013 32
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IEC 62396-3:2013(E) provides guidance and furthermore it provides necessary requirements for those involved in the design of avionic systems and equipment and the resultant effects of atmospheric radiation-induced single event effects (SEE) on those avionic systems. The outputs of the activities and objectives described in this part of IEC 62396 will become inputs to higher level certification activities and required evidences. It builds on the initial guidance on the system level approach to single event effects in IEC 62396-1:2012, considers some avionic systems and provides basic methods to accommodate SEE so that system development assurance levels are met.

PDF Catalog

PDF Pages PDF Title
4 CONTENTS
5 FOREWORD
7 INTRODUCTION
8 1 Scope
2 Normative references
3 Terms and definitions
12 4 Process guidance
13 5 Atmospheric radiation and electronic system faults
5.1 Atmospheric radiation effects on avionics
14 5.2 Hard faults
15 5.3 Soft faults
6 Aircraft safety assessment
6.1 Methodology
16 6.2 Mitigation
6.3 Specific electronic systems
6.3.1 Level A systems
Tables
Table 1 – Failure effect and occurrence probability
19 6.3.2 Level B systems
20 6.3.3 Level C systems
6.3.4 Levels D and E systems
21 Annex A (informative) Design process flow diagram for SEE rates
22 Annex B (informative) Some mitigation method considerations for SEEs
26 Annex C (informative) Example systems
Figures
Figure C.1 – Electronic equipment (flight control computers)
27 Figure C.2 – Electronic equipment (flight director computers)
28 Figure C.3 – Electronic equipment (engine control)
Figure C.4 – Electronically powered surface
29 Figure C.5 – Hydro mechanical drive of surface – Electronic valve control
30 Bibliography
BS IEC 62396-3:2013
$142.49