SAE ARD 50067 : A2003
Withdrawn
AVIONICS OPERATING SYSTEM APPLICATION PROGRAM INTERFACE REQUIREMENTS
01-12-2013
05-01-2003
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Withdrawn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 | ADA PROGRAMMING LANGUAGE (ANSI/MIL STD 1815A-1983) (NO S/S DOCUMENT) |
| 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 |