GE INTELLIGENT PLATFORMS ABI-PMC-1
Specifications
ASF Functionality: Bus Controller (BC)
BC retry
Intermessage gap selectable
Minor frame timing and message scheduling
Multiple BC data buffers in a linked list structure
Programmable delay gaps and null BC blocks
Programmable RT no-response time-out
Customer Support
Driver and library upgrades
Extended warranties available
Over 18 operating systems supported on various platforms
Two-year warranty
Interface Connections
µM in DB15F to coupling harness (CA-2189)
BJ77F Triax connector to 1553 bus
Coupling harness to bus and I/O connectors
DB I/O connector
Map Monitoring
Mapped buffers read by host processor as time permits
Multiple linked buffers for each transmit/receive subaddress
Number of buffers per transmit/receive subaddress is programmable or user defi nable to account for various host speeds
Maximum power consumption(98% bus activity)single channel
- 5 V @ 1.5 A (1.0 A with bus inactive)
Mechanical
Length 6.0” Width 2.9”s
LenStandard PMC card
Multi-Purpose I/O
Bi-directional external trigger
External TTL/RS-422 system clock input
IRIG clock input (optional)
PMC Functionality
16-bit and 32-bit transfer modes
50 MB per second maximum transfer rate
Memory mapped
On-boardfi rmware storage via Flash memory
PCI bus is 2.1 compliant
Programmable DMA controller
Remote Terminals (RT)
31 RT and all subaddresses supported
Multiple RT data buffers in a linked list structure
Programmable RT response time and no response selection
Transmit/Receive buffers for each subaddress
Self Test
BIT-RAM and encoder/decoder test
Power-up test with status register report
Run-time health status register
Unit Test application for 1553 bus functionality
Sequential Monitoring
100% independent
Comprehensive error table readable at any time by host processor
Host driver selected messages are double buffered
Messages time stamped with a 1 µs 32-bit clock or optional 48-bit IRIG-B clock
Standard firmware performs broad error monitoring
Software and Documentation Support
Borland and Microsoft® C Compiler compatible
Hardware and Integrated Avionics Library documentation included on CD. Hard copies of the documentation are available upon request.
Integrated Avionics Library with source code
Low-level drivers for most operating systems
Standard commercial temperature
0°C to +60°C;= 95% rH non-condensing
Features
- 1 or 2 dual redundant 1553 channels featuring 100% independent operation as one of the following, - Bus Controller, - Remote Terminal, - Dual Function Bus Monitor
- Architecture, - On-the-fly data structures, - BC and RT linked lists, - High-speed DSP, - Flexible memory structure, - Flash memory
- Bus Controller, - Programmable frame lists, - BC-RT, RT-BC, RT-RT, - Mode codes, broadcasts, and time delays
- Bus Monitor, - Map monitoring, - Sequential monitoring, - Time stamped, - Double buffered, - Error tables, - Definable monitoring
- Mezzanine Card - IEEE P1386 compliant
- RT Functionality, - RT level protocol selection, - RT definition tables, - Programmable response time,
- Software Support, - Complimentary drivers for most, operating systems, - Integrated Avionics Library, including, source code
Datasheet
Extracted Text
GE Intelligent Platforms ABI-PMC MIL-STD-1553 Interface ABI-PMC (PCI Mezzanine Card) interface broad error monitoring. They als provide a Features provides a fl exible, full function, dual redun- comprehensive error table that the host pro- • 1 dual redundant 1553 channel featuring dant MIL-STD-1553 interface to the PCI cessor can read at any time. 100% concurrent and independent Mezzanine. This Advanced Bus Interface (ABI) operation as a: architecture provides concurrent and indepen- Hardware Overview - Bus Controller dent operation of a Bus Controller (BC), - 31 Remote Terminals GE Intelligent Platforms bases the ABI inter- 31 Remote Terminals (RT), and dual function - Dual Function Bus Monitor face upon an advanced high speed DSP, Bus Monitoring (BM). The ABIPMC interface programmable logic and dual port RAM. It • Bus Controller equips the PMC carrier with a complete 1553 delivers a highly reliable hardware platform - Programmable frame lists interface. This includes 1553A/1553B selec- that is feature rich and user friendly. Through - BC-RT, RT-BC, RT-RT tions, pointer-driven transmit and receive the 128 kB of dual port RAM, the host proces- - Mode codes, broadcasts, and time delays buffers and extensive programmable sor has access to set up, monitor, and change • RT Functionality event interrupts. the 1553 interface data structures at any time. - RT level protocol selection Link-list memory architecture allows the user - RT defi nition tables BC simulation structures consist of linked lists to structure interface memory usage for the - Programmable response time of 1553 command messages: BC-to-RT, RT- maximum in flexibility and usefulness. • Bus Monitor to-BC, RT-to-RT, mode code, broadcast and - Map monitoring time delay block transmissions. We define RT Software Support Overview - Sequential monitoring simulation as a simple series of pointers to RT GE distributed software includes host - Time stamped defi nition tables. The RT defi nition tables in processor device drivers to the dual port - Double buffered turn point to control data buffers. We defi ne control and data structures as well as an - Error tables the bus activity we want to monitor in both application layer to these structures. GE also - Defi nable monitoring the Map and Sequential monitoring modes. provides low-level drivers for most operating • Architecture This provides user defi ned linked lists of data systems, and the Integrated Avionics Library - On-the-fl y data structures buffers and sequential 1553 activity. The user with source code, with the interface at no - BC and RT linked lists can time stamp and/or double buffer the additional cost. - High-speed DSP 1553 activity. Both monitoring modes perform - Flexible memory structure - Flash memory • Mezzanine Card - IEEE P1386 compliant • Software Support - Complimentary drivers for most operating systems - Integrated Avionics Library, including source code ABI-PMC MIL-STD-1553 Interface Multi-Purpose I/O • Standard commercial temperature: 0°C to +60°C; Specifications ≤ 95% rH non-condensing • Bi-directional external trigger • IRIG clock input (optional) • Mechanical: ABI Functionality: Bus Controller (BC) - Standard PMC card • BC retry • External TTL/RS-422 system clock input - Length 6.0” Width 2.9” • Minor frame timing and message scheduling PMC Functionality • Intermessage gap selectable Software and Documentation Support • PCI bus is 2.1 compliant • Programmable delay gaps and null BC blocks • Low-level drivers for most operating systems • 50 MB per second maximum transfer rate • Multiple BC data buffers in a linked list structure • Integrated Avionics Library with source code • 16-bit and 32-bit transfer modes ® • Borland and Microsoft C Compiler compatible Remote Terminals (RTs) • Memory mapped • Hardware and Integrated Avionics Library docu- • 31 RTs and all subaddresses supported • Programmable DMA controller mentation included on CD. Hard copies of the • Transmit/Receive buffers for each subaddress • On-boardfi rmware storage via Flash memory documentation are available upon request. • Multiple RT data buffers in a linked list structure Interface Connections • Programmable RT response time, no-response Customer Support • μM in DB15F to coupling harness (CA-2189) selection and no-response time-out • Two-year warranty • Coupling harness to bus and I/O connectors • Extended warranties available Map Monitoring • DB I/O connector • Driver and library upgrades • Multiple linked buffers for each transmit/ • BJ77F Triax connector to 1553 bus • Over 18 operating systems supported on receive subaddress Interface Card Specifi cations various platforms • Mapped buffers read by host processor as • Maximum power consumption (98% bus activity) - time permits single channel: • Number of buffers per transmit/receive subaddress - 5 V @ 1.5 A (1.0 A with bus inactive is programmable or user defi nable to account for various host speeds Sequential Monitoring • 100% independent Configurations • Host driver selected messages are double buffered • Messages time stamped with a 1 μs 32-bit clock or optional 48-bit IRIG-B clock • Standard fi rmware performs broad error monitoring Model Number Configuration • Comprehensive error table readable at any time by host processor ABI-PMC-1 Single Channel 1553 to PMC interface Self Test IRIG IRIG B Time Receiver (add /I to product number) • Power-up test with status register report • BIT-RAM and encoder/decoder test • Run-time health status register • Unit Test application for 1553 bus functionality About GE Intelligent Platforms GE Intelligent Platforms, a General Electric Company (NYSE: GE), is an experienced high-performance technology company and a global provider of hardware, software, services, and expertise in automation and embedded computing. We offer a unique foundation of agile, advanced and ultra-reliable technology that provides customers a sustainable advantage in the industries they serve, including energy, water, consumer packaged goods, government and defense, and telecommunications. GE Intelligent Platforms is a worldwide company headquartered in Charlottesville, VA and is part of GE Home and Business Solutions. For more information, visit www.ge-ip.com. GE Intelligent Platforms Contact Information Americas: 1 800 433 2682 or 1 434 978 5100 Global regional phone numbers are listed by location on our web site at www.ge-ip.com/contact www.ge-ip.com ©2010 GE Intelligent Platforms, Inc. All rights reserved. All other brands or names are property of their respective holders. Specifications are subject to change without notice. 01.10 GFA-1372
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