IEEE DRAFT 896.10 : D4.0 JUL 95
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
STANDARD FOR FUTUREBUS+ SPACEBORNE SYSTEMS PROFILE "S"
10-12-1996
12-01-2013
CLAUSE
1. OVERVIEW
1.1 Scope
1.2 Applicability
1.3 How to use this standard
1.4 Why use this standard
2. APPLICABLE DOCUMENTS
2.1 Referenced documents
3. DEFINITIONS
3.1 Special word usage
3.2 Bus line and signal conditions
3.3 Futurebus + terminology
3.4 Conventions
3.5 Syntax
3.6 Futurebus + logo
4. PROFILE S REFERENCE SPECIFICATION
4.1 Introduction
4.2 Target Applications
4.3 Reference tables
4.4 Profile S Interoperability
4.5 Conformance testing
5. DETAILED SPECIFICATION, FUTUREBUS + LOGICAL LAYER
5.1 Arbitration
5.2 Parallel Protocol
6. UTILITY SIGNALS
6.1 User console interface (UCIF) master present
6.2 Trigger (TR1) and trigger 2 (TR2)
6.3 Run
6.4 Nuclear event direct
6.5 Power failure imminent
6.6 Power normal
6.7 Warmstart
7. FAULT TOLERANCE ASPECTS OF THE PARALLEL PROTOCOL AND
UTILITY SIGNALS
7.1 Error detection
7.2 Error isolation, logging and diagnostics
7.3 Error removal and recovery
8. SERIAL BUS
8.1 Serial bus physical layer
8.2 Serial bus link layer
8.3 Serial bus transaction layer
9. BUS/NODE MANAGEMENT AND CSRS
9.1 Addressing
9.2 Byte-lane wiring and byte ordering
9.3 CSRs
9.4 Futerers + CSRs
9.5 Unit space CSRs
9.6 Conflicting standards
9.7 Serial bus management
9.8 Private space
9.9 Interrupts
9.10 Diagnostics and test
9.11 Monarch selection
10. DETAILED SPECIFICATION, PHYSICAL LAYER - SEM-E
STRETCH
10.1 Mechanical
10.2 Input/output
10.3 Profile connector, power and signal pin
11. DETAILED SPECIFICATION, PHYSICAL LAYER - 10 SU
11.1 Mechanical
11.2 Input/output
11.3 Profile connector, power and signal pin
assignments
12. PROFILE ELECTRICAL
12.1 Backplane characteristics and design
requirements
12.2 Module electrical characteristics and design
requirements
13. PROFILE S POWER
13.1 Module power
13.2 Host system power supplies
14. PROFILE S ENVIRONMENTAL SPECIFICATIONS
14.1 System environment requirements
14.2 Module environment requirements
15. RECOMMENDED PRACTICES
15.1 Thermal considerations
15.2 Power consumption
15.3 Pinouts
15.4 Bus performance analysis
15.5 Bandwidth considerations
16. PROFILE S MODULE SELECTION CRITERIA
16.1 Introduction
16.2 Profile S modules
16.3 Profile S systems
17. ALTERNATE PROFILE S MODULE CONNECTOR
ANNEX A. BIBLIOGRAPHY
Establishes a modular open architecture for spaceborne computing systems employing digital computers, processors, and other electronic modules. It provides for the integration and interoperability of diverse sets of electronic modules for the purpose of configuring various types of spaceborne computer systems. Specifies the electrical, logical, mechanical, thermal, and input/output interfaces necessary to allow modules, developed to this standard, to operate together in an integrated system or subsystem. In particular, the issues unique to spaceborne systems, such as size, weight, power, environment, reliability, and fault tolerance, are addressed.
DocumentType |
Draft
|
PublisherName |
Institute of Electrical & Electronics Engineers
|
Status |
Withdrawn
|
IEEE 896.2-1991 | IEEE Standard Backplane Bus Specification for Multiprocessor Architectures: Futurebus+(R) |
IEEE DRAFT 896.6 : D3 DEC 94 | FUTUREBUS+ TELECOMMUNICATIONS PROFILE |
MIL-STD-1540 Revision D:1999 | TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES |
MIL-STD-1547 Revision B:1992 | ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES |
IEEE DRAFT 1394 : D8.0V2 JUL 95 | HIGH PERFORMANCE SERIAL BUS |
MIL-STD-1773 Base Document:1988 | FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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