ARINC 653P3-2006 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3 - CONFORMITY TEST SPECIFICATION《航空电子设备软件标准接口部分3一致性试验规格》.pdf
《ARINC 653P3-2006 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3 - CONFORMITY TEST SPECIFICATION《航空电子设备软件标准接口部分3一致性试验规格》.pdf》由会员分享,可在线阅读,更多相关《ARINC 653P3-2006 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3 - CONFORMITY TEST SPECIFICATION《航空电子设备软件标准接口部分3一致性试验规格》.pdf(386页珍藏版)》请在麦多课文档分享上搜索。
1、 AN DOCUMENT Prepared by AIRLINES ELECTRONIC ENGINEERING COMMITTEE Published by AERONAUTICAL RADIO, INC. 2551 RIVA ROAD, ANNAPOLIS, MARYLAND 21401-7435 AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3 CONFORMITY TEST SPECIFICATION ARINC SPECIFICATION 653P3 PUBLISHED: October 16, 2006 DISCLAIM
2、ER THIS DOCUMENT IS BASED ON MATERIAL SUBMITTED BY VARIOUS PARTICIPANTS DURING THE DRAFTING PROCESS. NEITHER AEEC NOR ARINC HAS MADE ANY DETERMINATION WHETHER THESE MATERIALS COULD BE SUBJECT TO VALID CLAIMS OF PATENT, COPYRIGHT OR OTHER PROPRIETARY RIGHTS BY THIRD PARTIES, AND NO REPRESENTATION OR
3、WARRANTY, EXPRESS OR IMPLIED, IS MADE IN THIS REGARD. AEEC USES REASONABLE EFFORTS TO DEVELOP AND MAINTAIN THESE DOCUMENTS. HOWEVER, NO CERTIFICATION OR WARRANTY IS MADE AS TO THE TECHNICAL ACCURACY OR SUFFICIENCY OF THE DOCUMENTS, THE ADEQUACY, MERCHANTABILITY, FITNESS FOR INTENDED PURPOSE OR SAFET
4、Y OF ANY PRODUCTS, COMPONENTS, OR SYSTEMS DESIGNED, TESTED, RATED, INSTALLED OR OPERATED IN ACCORDANCE WITH ANY ASPECT OF THIS DOCUMENT OR THE ABSENCE OF RISK OR HAZARD ASSOCIATED WITH SUCH PRODUCTS, COMPONENTS, OR SYSTEMS. THE USER OF THIS DOCUMENT ACKNOWLEDGES THAT IT SHALL BE SOLELY RESPONSIBLE F
5、OR ANY LOSS, CLAIM OR DAMAGE THAT IT MAY INCUR IN CONNECTION WITH ITS USE OF OR RELIANCE ON THIS DOCUMENT, AND SHALL HOLD ARINC, AEEC, AND ANY PARTY THAT PARTICIPATED IN THE DRAFTING OF THE DOCUMENT HARMLESS AGAINST ANY CLAIM ARISING FROM ITS USE OF THE STANDARD. THE USE IN THIS DOCUMENT OF ANY TERM
6、, SUCH AS SHALL OR MUST, IS NOT INTENDED TO AFFECT THE STATUS OF THIS DOCUMENT AS A VOLUNTARY STANDARD OR IN ANY WAY TO MODIFY THE ABOVE DISCLAIMER. NOTHING HEREIN SHALL BE DEEMED TO REQUIRE ANY PROVIDER OF EQUIPMENT TO INCORPORATE ANY ELEMENT OF THIS STANDARD IN ITS PRODUCT. HOWEVER, VENDORS WHICH
7、REPRESENT THAT THEIR PRODUCTS ARE COMPLIANT WITH THIS STANDARD SHALL BE DEEMED ALSO TO HAVE REPRESENTED THAT THEIR PRODUCTS CONTAIN OR CONFORM TO THE FEATURES THAT ARE DESCRIBED AS MUST OR SHALL IN THE STANDARD. ANY USE OF OR RELIANCE ON THIS DOCUMENT SHALL CONSTITUTE AN ACCEPTANCE THEREOF “AS IS” A
8、ND BE SUBJECT TO THIS DISCLAIMER. 2006 BY AERONAUTICAL RADIO, INC. 2551 RIVA ROAD ANNAPOLIS, MARYLAND 21401-7435 USA Prepared by the Airlines Electronic Engineering Committee Specification 653 Adopted by the Airlines Electronic Engineering Committee October 4, 2005 ARINC SPECIFICATION 653P3 AVIONICS
9、 APPLICATION SOFTWARE STANDARD INTERFACE PART 3 CONFORMITY TEST SPECIFICATION Published: October 16, 2006i FOREWORD Aeronautical Radio, Inc., the AEEC, and ARINC Standards Aeronautical Radio, Inc. (ARINC) was incorporated in 1929 by four fledgling airlines in the United States as a privately-owned c
10、ompany dedicated to serving the communications needs of the air transport industry. Today, the major U.S. airlines remain the Companys principal shareholders. Other shareholders include a number of non-U.S. airlines and other aircraft operators. ARINC sponsors aviation industry committees and partic
11、ipates in related industry activities that benefit aviation at large by providing technical leadership and guidance and frequency management. These activities directly support airline goals: promote safety, efficiency, regularity, and cost-effectiveness in aircraft operations. The Airlines Electroni
12、c Engineering Committee (AEEC) is an international body of airline technical professionals that leads the development of technical standards for airborne electronic equipment-including avionics and in-flight entertainment equipment-used in commercial, military, and business aviation. The AEEC establ
13、ishes consensus-based, voluntary form, fit, function, and interface standards that are published by ARINC and are known as ARINC Standards. The use of ARINC Standards results in substantial benefits to airlines by allowing avionics interchangeability and commonality and reducing avionics cost by pro
14、moting competition. There are three classes of ARINC Standards: a) ARINC Characteristics Define the form, fit, function, and interfaces of avionics and other airline electronic equipment. ARINC Characteristics indicate to prospective manufacturers of airline electronic equipment the considered and c
15、oordinated opinion of the airline technical community concerning the requisites of new equipment including standardized physical and electrical characteristics to foster interchangeability and competition. b) ARINC Specifications Are principally used to define either the physical packaging or mounti
16、ng of avionics equipment, data communication standards, or a high-level computer language. c) ARINC Reports Provide guidelines or general information found by the airlines to be good practices, often related to avionics maintenance and support. The release of an ARINC Standard does not obligate any
17、airline or ARINC to purchase equipment so described, nor does it establish or indicate recognition or the existence of an operational requirement for such equipment, nor does it constitute endorsement of any manufacturers product designed or built to meet the ARINC Standard. In order to facilitate t
18、he continuous product improvement of this ARINC Standard, two items are included in the back of this volume: An Errata Report solicits any corrections to the text or diagrams in this ARINC Standard. An ARINC IA Project Initiation/Modification (APIM) form solicits any recommendations for addition of
19、substantive material to this volume which would be the subject of a new Supplement. ARINC SPECIFICATION 653 TABLE OF CONTENTS 1 INTRODUCTION.1 1.1 PURPOSE OF COMPLIANCE DEMONSTRATION .1 1.2 COMPLIANCE DEMONSTRATION CONCEPT .1 1.2.1 IMPLEMENTATION LEVELS AND SCOPE 1 1.2.2 PROPOSED PROCESS FOR DEMONST
20、RATION OF COMPLIANCE.2 1.3 Relationship to POSIX and the Open Group 5 2 GUIDELINES FOR IMPLEMENTATION OF TEST SPECIFICATION AND PROCEDURES.6 2.1 Test Procedures Determination6 2.2 ORGANIZATION OF THE DOCUMENT 7 3 Conformity Test Requirements9 3.1 ARINC 653 System Capability Requirements.9 3.1.1 Syst
21、em API/OS Compliance .9 3.1.2 Generic API/OS Management Types 10 3.2 Partition Services .10 3.2.1 Partition Management Types 11 3.2.1.1 Partition Management Types Requirements 11 3.2.1.2 Partition Management Types Test Procedures.11 3.2.2 Partition Management Services.12 3.2.2.1 GET_PARTITION_STATUS
22、.12 3.2.2.1.1 GET_PARTITION_STATUS Requirements 12 3.2.2.1.2 GET_PARTITION_STATUS Functional Test Procedures.13 3.2.2.1.3 GET_PARTITION_STATUS Robustness Test Procedures.13 3.2.2.1.4 GET_PARTITION_STATUS Service Macro13 3.2.2.2 SET_PARTITION_MODE 14 3.2.2.2.1 SET_PARTITION_MODE Requirements14 3.2.2.
23、2.2 SET_PARTITION_MODE Functional Test Procedures.17 3.2.2.2.3 SET_PARTITION_MODE Robustness Test Procedures 21 3.2.2.2.4 SET_PARTITION_MODE Service Macro .22 3.3 Process Services .22 3.3.1 Process Management Types.22 3.3.1.1 Process Management Types Requirements.22 3.3.1.2 Process Management Types
24、Test Procedures.24 3.3.2 Process Management Services.25 3.3.2.1 GET_PROCESS_ID.25 3.3.2.1.1 GET_PROCESS_ID Requirements 25 3.3.2.1.2 GET_PROCESS_ID Functional Test Procedures.26 3.3.2.1.3 GET_PROCESS_ID Robustness Test Procedures.26 3.3.2.1.4 GET_PROCESS_ID Service Macro26 3.3.2.2 Get_Process_Status
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