SIST EN 4660-005:2011

Oznaka standarda: SIST EN 4660-005:2011
Koda projekta: 04003275
Organizacija: SIST
Naslov (angleški): Aerospace series - Modular and Open Avionics Architectures - Part 005: Software
Naslov (slovenski): Aeronavtika - Modularne in odprte letalske elektronske arhitekture - 005. del: Programska oprema
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Ime Jezik Status Cena Dodaj v košarico
SIST EN 4660-005:2011 angleški jezik Withdrawn SIST-2C: 223.30 EUR
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Tehnični odbor: I13 - Imaginarni 13
ICS: 49.090
Status: Razveljavljen
Objavljen: 01-okt-2011
Refer. št. objave: Sporočila 2011-10
Razveljavitev: 01-okt-2019
Referenca razveljavitve: Sporocila 2019-10
Področje projekta (angleško): The purpose of this 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). 1.2.6 Module Support Layer (MSL) (...)
Področje projekta (slovensko): Namen tega evropskega standarda je vzpostaviti enotne zahteve za načrtovanje in razvoj programske arhitekture za modularne letalske sisteme, kot je opredeljeno v ASAAC.
Povezava na standarde
Povezava Ime Datum
Revidiran SIST EN 4660-005:2019 - Aeronavtika - Modularne in odprte letalske elektronske arhitekture - 005. del: Programska oprema 04-feb-2015
Nadomeščen z SIST EN 4660-005:2019 - Aeronavtika - Modularne in odprte letalske elektronske arhitekture - 005. del: Programska oprema 28-avg-2019


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