SAE ARD 50067 : A2003
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
AVIONICS OPERATING SYSTEM APPLICATION PROGRAM INTERFACE REQUIREMENTS
01-05-2003
12-01-2013
1 SCOPE
1.1 Purpose
1.2 Introduction
1.3 Terminology
1.4 Document Overview
2 APPLICABLE DOCUMENTS
2.1 Government Documents
2.2 Non-Government Documents
2.3 Definitions
3 ENGINEERING REQUIREMENTS
3.1 Synchronization Interface Requirements
3.2 Program Support
3.3 Task Control
3.4 Data Security
3.5 Memory Management
3.6 Communication
3.7 Timer Services
3.8 File Management
3.9 Input/Output
3.10 Special devices
3.11 Configuration
3.12 Fault management
3.13 Built in test (BIT)
3.14 Instrumentation
3.15 Non operational support
3.16 Bootup/initialization/shutdown
3.17 Reinitialization
4 Acronyms
Appendix A
Intended to gather avionics Operating System interface requirements in order to develop an Application Program Interface (API). Aims to address the avionics community and possibly address other real-time embedded applications.
| Committee |
AS-5
|
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Withdrawn
|
| SAE AS4893A | Generic Open Architecture (GOA) Framework |
| MIL-STD-1815 Revision A:1983 | |
| IEEE DRAFT 1003.21LIS : D3.0 99 | DRAFT STANDARD FOR INFORMATION TECHNOLOGY - PORTABLE OPERATING SYSTEMS INTERFACE (POSIX) - PART 1: REALTIME DISTRIBUTED SYSTEMS COMMUNICATION APPLICATION PROGRAM INTERFACE (API) [LANGUAGE-INDEPENDENT] |
| ISO/IEC 8652:2012 | Information technology — Programming languages — Ada |
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