Application requirements for CAN bus of electronic system in missile/launch vehicle
1 Scope
This standard specifies the design method, working mode, application layer protocol, network topology and interface, cable requirements, test requirements, etc. for CAN bus of electronic system in missile/launch vehicle.
This standard is applicable to the design, production, test and acceptance of CAN bus of electronic system in missile/launch vehicle.
2 Normative references
The following normative documents contain provisions which, through reference in this text, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions, of any of these publications do not apply to this standard. However, parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the latest edition of the document referred to applies.
ISO 11898-2 Road vehicles - Controller area network (CAN) - Part 2: High-speed medium access unit
ISO 16845 Road vehicles - Controller area network (CAN) - Conformance test plan
3 Terms, definitions and abbreviations
3.1 Terms and definitions
For the purposes of this standard, the terms and definitions given in ISO 11898-2 and the following apply.
3.1.1
terminal
electronic component of bus and subsystem interface
3.1.2
protocol
rules for exchanging information through interfaces
Foreword i
1 Scope
2 Normative references
3 Terms, definitions and abbreviations
4 Bus design requirements
5 Working mode
6 Application layer protocol
7 Network topology and terminal connection mode
8 Requirements for cable and interface
9 Redundancy design requirements
10 Requirements for bus test and fault handling
Annex A (Informative) CAN bus characteristics
