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BS EN 4660-005:2011

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Aerospace series. Modular and open avionics architectures Software

Available format(s)

Hardcopy , PDF

Superseded date

28-08-2019

Superseded by

BS EN 4660-005:2019

Language(s)

English

Published date

31-05-2011

€574.95
Excluding VAT

0 Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviations
4 System Functions
5 Software Architecture Definition
6 Direct Interfaces Definitions
7 Logical Interfaces Definitions
8 Data Type Definitions
9 Tailoring
Annex A (normative) - AGL

Specifies uniform requirements for design and development of software architecture for modular avionics systems as defined per ASAAC.

Committee
ACE/6
DocumentType
Standard
Pages
510
PublisherName
British Standards Institution
Status
Superseded
SupersededBy

The purpose of this European Standard is to establish uniform requirements for design and development of software architecture for modular avionics systems as defined per ASAAC. 1.1 Software Architecture Overview The ASAAC Software Architecture is based on a three-layer stack as shown by a simplified Figure 2. Each layer is described in terms of it dependency/independency on both the aircraft system and the underlying hardware. 1.2 Software Architectural Components Figure 3 provides an overview of the software architectural components and software interfaces. 1.2.1 Functional Applications The term \'Functional Applications\' relates to all functions that handle the processing of operational data, e.g. - Radar Applications, - Mission Management, - Stores Management, - Vehicle Management System, - Communication, Navigation and Identification. 1.2.2 Application Management (AM) AM is responsible for the non-standardised system management, i.e. the AM performs the non-generic system management. As an example, the AM may perform the mission/moding management. The interface between the AM and GSM is the System Management Logical Interface (SMLI) (see 4.1.2). 1.2.3 Operating System (OS) A Real-Time OS provides the particular part of OSL functionality that controls the real-time behaviour of the Processing Element and its associated resources (see Clause 0). 1.2.4 Generic System Management (GSM) The GSM is responsible for the management of the core processing (see 4.1.1 and 5.2.1). This functionality is divided into four areas: - Health Monitoring, - Fault Management, - Configuration Management, - Security Management. 1.2.5 Run-Time Blueprints (RTBP) The RTBP contain the information (e.g. process description, routing information, fault management data) required to configure and manage the core processing on which it is hosted (see 5.3). (...)

Standards Relationship
EN 4660-005:2011 Identical

EN 4660-004:2011 Aerospace series - Modular and Open Avionics Architectures - Part 004: Packaging
EN 4660-002:2011 Aerospace series - Modular and Open Avionics Architectures - Part 002: Common Functional Modules
EN 4660-003:2011 Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network
EN 4660-001:2011 Aerospace series - Modular and Open Avionics Architectures - Part 001: Architecture
ISO/IEC 14977:1996 Information technology — Syntactic metalanguage — Extended BNF

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