Document History Version Cover Date Created by Description 1.00 July 10, 1999 Douglas Ullah and Creation of Document Hansjoerg Frey 1.01 Jult 10, 1999 Reformated
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Flying High with STANAG3910 Overview and History As the EF2000 Typhoon enters the production stage of its development, STANAG3910, EFAbus will get its first chance to prove itself by meeting the mission critical avionics requirements for this highly sophisticated fighter aircraft. Since it was established at the early stages of the programme that the data transfer capacity of the MIL-STD-1553B bus was not going to fulfil the requirements, STANAG3910 was selected by the Eurofighter (UK, Germany, Italy & Spain) consortium in 1989 to meet the demanding Avionics Systems needs of such an aircraft. Very simply STANAG3910, EFAbus is based on using the existing MIL-STD-1553B, 1Mbit/sec dual redundant Low Speed (LS) bus augmented by a High Speed, (HS) Fibre Optics (Reflexive Star Topology) dual redundant bus operating at 20Mbits/sec. The LS bus provides the command and control of the HS bus by use of Action Words sent over the LS bus. The HS bus is used only for Data Transfers under the control of these Action Words. The bus architecture comprises a Bus Controller (BC) with up to 31 Remote Terminals (RTs). Each device can have a LS/HS connection as shown in Figure 1. Bus Concept Bus Remote Remote Bus Controller Terminal Terminal Monitor LS-BIU HS-BIU LS-BIU HS-BIU LS-BIU LS-BIU HS-BIU
Dual Redundant LS-Bus (Electrical)
F/O F/O Reflexive Reflexive Star Coupler Star Coupler Dual Redundant HS-Bus (Optical)
In the case of the EF2000 implementation, RT Sub-address 26 (decimal) on the LS bus is reserved as the HS Sub-address. All HS transfers are initiated via the LS bus with Command and Status words for the HS bus being transferred as LS datawords. The transfer types are as defined in the MIL-STD-1553B with no automatic acknowledgement of HS data transfers in the basic protocol. Therefore HS RT status must be polled by the transmitting terminal. It will be seen that this dual bus approach allows the mixed operation of both STANAG3910 and MIL-STD-1553B terminals. The first draft of this dual speed MIL-STD-1553B based bus was created in Germany during 1987. In 1988, this first draft was submitted to the AVS WP in Brussels. Following this in 1989, a project specific variant known as EFAbus was issued. This is the version used today (with some updates) for the EF2000 aircraft project. STANAG3910 Overview Page 5
GmbH It should be appreciated that this standard was adopted due to the lack of a truly available off the shelf High Speed Data Bus for Avionics applications. This, in conjunction with the reasons listed below, drove the down selection of the STANAG3910, EFAbus for the EF2000, Typhoon aircraft: • Allow evolution from MIL-STD-1553B bus only to Higher Speed Avionics Bus System • Mixing of MIL-STD-1553B/ STANAG3910 Avionics Systems • Low Risk approach with first EF2000 Prototypes using MIL-STD-1553B only • Stay with a Deterministic Master/ Slave Protocol Physical Layer of the HS Bus The implementation using Fibre Optic technology STANAG3910 HS bus was to eliminate Electro Magnetic Interference (EMI) and reduce the susceptibility to lightning, radiation and Nuclear Electro Magnetic Pulses (NEMP). The STANAG3910 standard defines the physical layer of the HS bus for both Electrical and Fibre Optical implementations. The fibre optic topologies can be implemented in several ways: • Transmisive Star • Reflexive Star (used for EF2000, Typhoon) • Linear Bus Figure 2 showss a Transmissive Star Coupled bus. The advantages to this topology is that you have a favourable Optical Power Budget with a similar Optical Input Signal level for all Terminals. The disadvantages are that expansion is very difficult and two fibre optical cables are required (four fibres per dual redundant Terminal).
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TX Terminal #1 RX
TX Terminal #2 RX TX Terminal #n RX
Transmissive Star Coupler
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GmbH Figure 3 shows a Reflexive Star Coupled bus topology. The advantages of such a topology include a reasonable Power Budget, similar optical input power for all Terminals and a minimal fibre optic-cabling requirement. The disadvantages are that expansion is very difficult and an Optical Splitter is required in each Terminal. TX Terminal #1 RX Splitter TX Terminal #2 RX Splitter
TX Terminal #n RX Splitter
Figure 4 shows a Linear Tee Coupled Bus. The advantages of such a topology are that expansion is easy. However the disadvantage is that the receiver input signal level is position dependant which means receiver must have a wide dynamic range, hence it has a bad Optical Power Budget.
Coupler
Coupler
Coupler
Coupler
TX Terminal #1 RX
TX Terminal #2 RX TX Terminal #n RX
Coupler
Coupler
Reflective Star Coupler
GmbH The Reflexive Star Optical implementation selected for the EF2000 uses the following parameters: • Wavelength 770850 nm • Transmitter Output -0.5 +/- 3.5dbm (peak) • Receiver Sensitivy - 37 dbm (peak) • Bit Error Rate < 10 10 • Fibre 200/280 µ m, step index, numerical aperture 0.24 Transfer Protocol Specifically the LS bus handles the transfer protocol. Once the LS Bus Controller further has initiated an HS LS BC messages can be initiated. STANAG3910 defines several HS transfer types, which are shown in the figures below: LS Bus Command HS Action Status Next Word Word * * Word # # Transfer ST I HS Message Frame H Bus
* * : MIL-STD-1553B Response Time ( 4 ... 12 µs ) # # : MIL-STD-1553B Intermessage Gap ( > 4 µs ) T I : HS Transmitter Initialise Time (24 ... 32 µs ) Figure 5 HSBC and RT to BC Transfer
LS Bus Command HS Action Next Word Word # # Transfer HS Bus T I HS Message Frame
Figure 6 HS BC Broadcast Transfer
## : MIL-STD-1553B Intermessage Gap ( > 4 µs ) T I : HS Transmitter Initialise Time ( 24 ... 32 µs ) Page 8
GmbH LS Bus Command HS Action Status Command HS Action Status Next Word Word (RX) * * Word # # Word Word (TX) * * Word # # Transfer
R I /R IOUT
T I HS Message Frame
HS Bus * * : MIL-STD-1553B Response Time ( 4 ... 12 µs ) ## : MIL-STD-1553B Intermessage Gap ( > 4 µs ) T I : HS Transmitter Initialise Time (24 ... 32 µs ) Figure 7 HS RT to RT LS Bus Command HS Action Command HS Action Status Next Word Word (RX) # # Word Word (TX) * * Word # # Transfer
HS Bus
T I HS Message Frame R I /R IOUT
Figure 8 HS RT Broadcast HS Mode Code transfers use the BC to RT or BC Broadcast transfer of one action word and optionally one data word. At this point in time the standard does not define HS Mode Codes with an additional data word. The Mode Codes currently defined are as follows: Hex Value HS Mode Code 03 Initiate HS Self Test 04 HS Transmitter Shutdown 05 Override HS Transmitter Shutdown 08 Reset HS Terminal 09 HS Receiver Initialise OA HS Transmitter Initialise To perform an HS Status check a RT to BC transfer has to be issued via the LS bus. The Word Count maybe variable but no transactions take place on the HS bus. The HS Status Word is in the first data word, HS Action Word in the second word and the HS Built in Test (BIT) in the third word. With regards with BIT word, STANAG3910 EFAbus does not define the usage of these bits.
STANAG3910 Overview Page 9
GmbH Figure 9 shows the HS Status Check sequence sent on the LS bus. Command Status HS Status Last HS HS BIT Data Data Word Word Word Action Word Word Word 1 Word 1 * * Both the LS and HS buses have strict Protocol timing requirements defined. In the case of the LS bus this is the same as STANA3838 (equivalent to MIL-STD-1553B). For the HS bus the following protocol timing requirements are defined: Transmitter Initialise Time 2432 µ s Receiver Initialise Time 24 µ s max. Receiver Initialise Timeout 185 +/- 15 µ s Data Streaming Timeout 4.15 ms +/- 20% Inter Transmission Gap 2 µ s HS Action Word The HS Action Word is a data word sent by the BC to HS Sub-Address of one or all Terminals on the LS bus. It controls any HS data transfer and contains any HS Mode Code specification as required by the BC. The HS action word is always a One Word Message on the LS bus generated by the BC. The HS Action words for Data Transfers and Mode Codes are shown in Figures 10 & 11. MSB LSB 15 14 13 7 6 0 HS A/B HS T/R HS Message Identify HS Block Count Figure 10 • HS A/B: HS Bus Select 0: use HS Bus A 1: use HS Bus B • HS T/R: HS Transfer Direction 0: Receive 1: Transmit • HS Message Identify: 7 Bit HS 'Subaddress' • HS Block Count: Number 32 Word blocks contained in HS Message Frame MSB LSB 15 14 13 7 6 0 HS A/B HS T/R 0 0 0 0 0 0 0 HS Mode Code Figure 11 • HS A/B: HS Bus Select 0: use HS Bus A 1: use HS Bus B • HS T/R: HS Transfer Direction 0: Receive 1: Transmit • HS Mode Code : - 6 HS Mode Codes are defined, for all of them Broadcast is allowed - 9 Mode Codes are reserved - 2 reserved Mode Codes with Data Word Page 10
GmbH
HS Status Word The HS Status Word definition is shown in Figure 12 below. MSB LSB 15 14 9 8 3 2 0 HS TF HS Receiver Status HS Transmitter Status Reserved Figure 12 • HS TF: HS Terminal Flag ( optional ) HS RX Status Bit 14 : HS Message Frame Error • Bit 13 : HS Receiver Active Bit 12 : HS Receiver not ready ( optional) Bits 9...11: reserved (set to 0) • HS TX Status Bit 3 : HS Transmitter active Bit 4: HS Transmitter not readies (optional) Bits 5...8: reserved (set to 0) HS Message Frame The HS Message Frame contains several elements, which are common with the SAE HS Bus Standard. The HS frame length is a minimum of 624 bits up to a maximum of 65,648 bits depending on the type of HS message transfer, which takes place. It contains a Preamble, Start Delimiter, Headers, Word Count, Information field, Error Detection (CRC) and an End Delimiter. Figure 13 below shows the make up of the HS Message Frame Preamble SD FC PA DA WC INFO CRC ED Figure 13 The following describes the elements, which make up the HS Message Frame Preamble - This is 40 bits of Manchester Encoded logic 1s (20Mhz square wave signal) and is used for gain control of the receivers, receiver clock recovery and the decoding of the Start of Frame. Start Delimiter - This is 8 bits of Manchester Code Violations and contains a unique pattern to identify the start of HS frame. Bit 0 Bit 1 Bit 2 Bit 3