1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref
2、rom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2016 SAE InternationalAll rights reserved. No part of this publi
3、cation may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on thisTechnical Report, please visithttp:/standards.sae.org/AIR6520AEROSPACEINFORMATION REPORTAIR6520Issued 2016-12Unmanned Systems (UxS) Control Segment (UCS) Archite
5、cture: Version Description DocumentRATIONALEThis document describes the correspondence between the SAE UCS Architecture (AS6512) Library and the United States Office of the Secretary of Defense (OSD) UAS Control Segment (UCS) Architecture Library Release 3.4(PR) approved for Distribution A public re
6、lease 15.S-1859.1. SCOPEGovernance of the Unmanned Aircraft System (UAS) Control Segment (UCS) Architecture was transferred from the United States Office of the Secretary of Defense (OSD) to SAE International in April 2015. Consequently, a subset of the UCS Architecture Library Release 3.4(PR) has b
7、een published under SAE as the Unmanned Systems (UxS) Control Segment (UCS) Architecture, AS6512. This Version Description Document (VDD) describes the correspondence and differences between the two architecture libraries.2. APPLICABLE DOCUMENTSThere are no referenced publications specified herein.3
8、. SUMMARY OF DOCUMENT UPDATES3.1 System-of-InterestUnder SAE, the name of the UCS Architecture has been changed from the OSD Unmanned Aircraft System (UAS) Control Segment (UCS) Architecture to the Unmanned Systems (UxS) Control Segment (UCS) Architecture. This reflects a strategic change in scope f
9、rom U.S. Department of Defense UAS Groups 2 through 5 to all UxS including military and non-military unmanned vehicles whose means of conveyance can be air, water, or ground. However, the current technical content of AS6512 is still based on Department of Defense use cases for UAS Groups 2 through 5
10、. No additional technical requirements have been added at this time. Support for additional unmanned systems would be provided by conformant user extensions to AS6518 as permitted by AS6513 (UCS Architecture: Conformance Specification).3.2 LibraryThe correspondence between the two architecture libra
11、ries is summarized in Table 1. In general, the original OSD configuration item was either retired or republished under SAE. The republication of an OSD configuration resulted in no technical changes from R3.4(PR) for users of R3.4(PR). Under SAE, the UCS Architecture Description (AS6512) serves as t
12、he formal definition of the UCS Architecture with the other documents in the UCS Architecture Library being a part of AS6512 by reference.SAE INTERNATIONAL AIR6520 Page 2 of 2Table 1 Correspondence between OSD UCS Architecture Library R3.4(PR) and SAE UCS Architecture as defined in AS6512OSD UCS Arc
13、hitecture R3.4 Configuration Item Corresponding SAE publicationUCS-INF-AD Version 2.4(PR) AS6512UCS-INF-VDD Version 1.4(PR) AIR6520UCS-SPEC-MODEL Version 3.4(PR) AS6518UCS-SPEC-TECHGOV Version 2.5(PR) AS6522UCS-SPEC-CONFORMANCE Version 2.5(PR) AS6513UCS-SPEC-UCSFACEDMM Version 1.0(PR) RetiredUCS-INF
14、-ICD Version 2.4(PR) AIR6514UCS-INF-ICD-SRC Version 2.4(PR) Included as archive file in AIR6514UCS-INF-ICD-EA Version 1.2(PR) AIR6515UCS-INF-ICD-RSA Version 1.2(PR) AIR6516UCS-INF-ICD-RPY Version 1.2(PR) AIR6517UCS-INF-UCTRACE Version 1.4(PR) AIR6519UCS-G-ICDDDS Version 2.4(PR) AIR6521UCS-PLN-AV1 Ve
15、rsion 3.4(PR) RetiredUCS-PLN-GOV Version 3.3(PR) Retired (replaced by SAE AS-4UCS internal document)UCS-STD-CAPIS Version 2.1(PR) RetiredUCS-G-MODELEX Version 1.3(PR) RetiredUCS-G-MIR Version 2.3(PR) RetiredUCS-G-ICDJMS Version 2.4(PR) Retired4. NOTES4.1 Revision IndicatorA change bar (I) located in
16、 the left margin is for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (R) are not used in original publications, nor in documents that contain editorial changes only.PREPARED BY SAE SUBCOMMITTEE AS-4UCS, UNMANNED AIRCRAFT SYSTEM CONTROL SEGMENT OFCOMMITTEE AS-4, UNMANNED SYSTEMS
