SAE AS 1393-2010 Serial Hi-Rel Ring Network for Aerospace Applications (RingNet)《航空航天设施用连续Hi-Rel环形网络(RingNet)》.pdf
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1、AEROSPACE STANDARD AS1393 Issued 2010-03 Reaffirmed 2014-10 Serial Hi-Rel Ring Network for Aerospace Applications (RingNet)RATIONALE AS1393 has been reaffirmed to comply with the SAE five-year review policy. _ SAE Technical Standards Board Rules provide that: “This report is published by SAE to adva
2、nce 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 therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least ev
3、ery five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2014 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by
4、 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 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.s
5、ae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS1393 INTRODUCTION Application perspective The bandwidth and resolution of aerospace remote-sensing payloads continue to advance, placing ever increasing demands on onboard
6、 data-handling networks. At the same time, economics and rapid development requirements are driving onboard data-handling networks toward flexible, nonproprietary architectures and interface standardization. These characteristics are extensively addressed in existing ground-based net- works. However
7、, unlike most ground-based networks designed primarily to support the transfer of non-real- time data between computers, an onboard data-handling network must support the real time needs of the aerospace remote-sensing environment. Network perspective Aerospace remote-sensing data is characterized b
8、y synchronous components, common to continuous mode sensors, and asynchronous components, common to event driven sensors. Both sensor types have real time data-handling requirements, and sensor performance is driving data bandwidth requirements into multiple gigabit per second range. Even at these h
9、igher data rates, aerospace systems will continue to be constrained by size, weight, and power limitations. In order to achieve high data-rate performance while maintaining low size, weight, and power, onboard data-handling subsystems must employ highly integrated components and must avoid the highe
10、r layer protocol features commonly found in ground-based networks. Furthermore, space-based data-handling networks must be fault tolerant and able to withstand the rigors of launch and the harsh space environment. Adaptation of existing ground-based network standards is not practical because of insu
11、fficient bandwidth and high power dissipation. Also, conversion of current implementations to space qualifiable processes is not feasible. Therefore, a new onboard data-handling network standard for aerospace remote-sensing applications is necessary. Technology perspective Fiber Optic and ASIC techn
12、ologies have matured to the point that multiple gigabit data-handling networks for aerospace applications are practical. Fiber Optic technology is especially appealing because of its extremely high bandwidth capacity. Multimode fibers have been demonstrated to be radiation hard with negligible incre
13、ase in signal loss over a ten year life in space radiation environments. Space qualifiable connectors have been designed and built specifically for fiber cable. Techniques for low loss termination and coupling of fibers have been perfected. High power laser diodes capable of operation over a wide te
14、mperature range and low noise optical receivers are now available. State-of-the-art semiconductor materials and processes, as well as packaging techniques, are leading towards smaller, faster, and lower power devices that will enable high-speed data-handling systems for space applications. TABLE OF
15、CONTENTS 1. SCOPE . 9 1.1 Purpose 9 2. References . 9 2.1 Applicable Documents . 9 2.2 List of Acronyms . 9 2.3 Definitions 10 3. Network Description . 12 3.1 Overview 12 3.1.1 Topology 12 3.1.1.1 Addressing . 12 3.1.2 OSI Protocol Layer Allocation 12 3.1.3 Network Characteristics . 14 3.1.3.1 Physi
16、cal Layer Characteristics . 14 3.1.3.2 Data Link Layer Characteristics . 14 3.1.3.3 Management Layer Characteristics . 16 3.2 Operation . 17 3.2.1 Control Node Interface . 17 3.2.1.1 Discrete Command and Control Interfaces 17 3.2.1.2 Register Interfaces . 18 3.2.1.3 CCIR Structure and Definition 19
17、3.2.1.4 CIU Single Command Definitions 22 3.2.1.5 CIU Block Command Definitions 24 3.2.1.6 Block Load Command Execution . 26 3.2.1.7 Initialize Command i.e., the fiber optic cables and connectors. The BIU, or Bus Interface Unit, is intended to be an embedded module within each Data Node. It provides
18、 the primary data handling functions required to both send and receive data over the RingNet network. The CIU, or Control Interface Unit, is intended to be an embedded module within a Control Node. It provides the primary configuration, control and status monitoring interface to the RingNet network.
19、 FIGURE 3-1 - RINGNET TOPOLOGY 3.1.1.1 Addressing Address 0x7F is reserved for broadcast commands and address 0x7E is reserved for the optional Bus Monitor function, limiting the number of BIUs to 125. Address 0x00 is reserved for the CIU. The remainder of the addresses (0x01 0x7D) can be used for B
20、IU addresses. 3.1.2 OSI Protocol Layer Allocation In an effort to standardize the protocol structure, the International Standards Organization (ISO) created the 7layer Open System Interconnection (OSI) model to define and partition the basic network processes (see Table 1). The RingNet network incor
21、porates the three layers of this 7layer model associated with data transfer, the Physical Layer, Data Link layer and Network Layer. The RingNet also provides a limited set of Network Management functions. These Network SAE INTERNATIONAL AS1393 Page 12 of 123_ Management functions have been combined
22、with the Network Layer functions to form the RingNet Management Layer. Figure 3-2 illustrates in a simplified form the allocation of these protocol layers to the RingNet functional element. Network Independent Layers 7- Application Layer Management Layer 6 - Presentation Layer 5 - Session Layer 4 -
23、Transport Layer Network Dependent Layers 3 - Network Layer 2 - Data Link Layer 1 - Physical Layer 1.1 - Non-Media Dependent Physical Layer 1.2 - Media Dependent Physical Layer TABLE 1 - ISO/OSI MODEL a) Physical Layer - In the RingNet the Physical Layer is divided into two parts, the Media Dependent
24、 Physical Layer (MDPL) and the Non-Medial Dependent Physical Layer (NMDPL). The passive elements of the MDPL, the network cable and connectors, are contained within the Physical Plant. The active elements of the MDPL associated with signaling and the NMDPL processes associated with symbol encoding a
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