head 1.4; access; symbols ref:1.1.1.1.0.2 arelease:1.1.1.1 GNU:1.1.1; locks; strict; comment @# @; 1.4 date 2005.05.18.00.34.17; author btltz; state Exp; branches; next 1.3; commitid 228c428a8d794567; 1.3 date 2005.05.03.16.13.54; author btltz; state Exp; branches; next 1.2; commitid 4f174277a33f4567; 1.2 date 2005.05.02.15.27.00; author btltz; state Exp; branches; next 1.1; commitid 3038427646934567; 1.1 date 2005.04.16.03.10.50; author btltz; state Exp; branches 1.1.1.1; next ; 1.1.1.1 date 2005.04.16.03.10.50; author btltz; state Exp; branches; next ; desc @@ 1.4 log @no message @ text @ --------------------------------------------- Introduction ------------------------------------------------------------------ ************************************ SpaceWire (SpW) for What? "Spw grown organically from the needs of on-board processing applications. SpW is a network with Routers. This Standard addresses the handling of payload data and control information on board a spacecraft. It is a standard for a high speed data link, which is intended to meet the needs of future, high capability, remote sensing instruments and other space missions. Processing units, mass-memory units and down-link telemetry systems developed for one mission can be readily used on another mission, reducing the cost of development, improving reliability and most importantly increasing the amount of scientific work that can be achieved within a limited budget. SpW is currently being installed on several NASA and European Space Agency (ESA) spaceships to support onboard communications during space missions.---27 January 2003) SpaceWire has taken into consideration two existing standards, IEEE 1355-1995 and ANSI/TIA/EIA-644. "Point-to-point serial links with LVDS. The maximum data signalling rate that can be achieved is different from one system to another, depending on several factors such as: 1)cable length, 2)driver-receiver technology, and 3)encoder-decoder design, and is limited by 4)skew and jitter." ********************************************* Diff & Relation with IEE1355 device(eg. Atmel.Inc "TSS901E" which also called "SMCS332") The initial SMCS(Scalable Multi-Channel Communications Subsystem) device is for use in multi- processor systems. Its further application examples are heterogeneous system without communication features. "The SMCS devices implement revision A of the standard, which is based on IEEE1355. They do not implement the current version of SpaceWire. However, the current version of SpaceWire is backwards compatible with the earlier revision." ------------------------------------------------ This Core ----------------------------------------------------------------- This Core? - CODEC - A pure synchronous design(so it can works well in fpga) written in verilog, completely open. - Annother high speed CODEC use PLL and clock recovery/lock circuit. - SWR - Synchronously Clocked Crosspoint (safe and easy to debug/test) - Buffered crossbar, distributed scheduling(effective and simple) which include "Column scheduler" and "Line Scheduler". 16x16 xbar now may be enough. - Provide only RR scheduling, coupled with 2 priority levels. * Due to the SpaceWire protocol,the file/module "SPW_CODEC.v" could be used as a core's top module (as a "channel") to be integrated with a "routing matrix" to form a router which is a Routing Switch in the SpaceWire network. Sometimes the CODEC is also called a "interface" or "input/output ports" of the router or a node device. See the scheme. * The file/module "SPW_I_vlogcore.v" is 3 CODEC with glue logic and Wishbone interface (COMI/HOCI) could be used as top module(a interface of the host to the SpW network) and be integrated into node devices. ("SpaceWire nodes are the sources and destinations of packets in a SpaceWire network."). * The file/module "SWR_vlogcore.v" is a top module of Spacewire Router which integrates some interfaces and a Routing Matrix "SwitchCore.v" and a little other logic. * Had use some ip on the opencores.org such as a fifo(i have consulted the "plesiochronous_fifo.v" for the Receiver. For the transmitter which only need a synchronous fifo for internal usage,so i write a synfifo which was similar to Xilinx ip for less complexity. The switch matrix use "eth_fifo" which is part of OC's project "Ethernet MAC") and a CRC. * Note the LVDS driver and receiver is instanced in modules use Xilinx primitives. You may change that if you use other FPGA vendor's devices. ---------------------------------------------- A little Specs: ---------------------------------------------------------- General: - The SpaceWire interface registers(RegSpW.v) could be accessed by WISHBONE HOCI (WISHBONE slave interface). The SpaceWire Router registers(RegSWR.v) could be accessed by "Configuration Port", through parallel "external port(s)" or the serial SpaceWire interfaces, ie. through the SpaceWire transceiver. ***************** -INTERFACE - The block "Timer" in the scheme of the draft-1 is merged into the "SPW_FSM". -[Clock] -Clock : Synchronous method - The block "Receiver's clock recovery" in the scheme of the draft-1 is merged into the "Receiver". - The block "Transmitter clock generator" in the scheme of the draft-1 is merged into the "Transmitter". -Clock : High speed method -The wide -> narrow process unit could be found in Transmitter and PPU. - - The credit count keeped in "crd_cnt" which indicates the buffer space of the opposite Rx bufer is in the transmitter; at the same time the outstanding count keeped in "osd_cnt" which indicates the buffer data of the opposite Tx is in the receiver. - Notice that according to the custom of circuit operation,some names near the interface between the Tx/Rx and the fifo may be a little different from the standard document.(eg."TX_READY, TX_WRITE" may only present as a output pulse signal "rdbuf_o" to just read that memory. - Note that the Receiver could generate local EEP to the host. It also could receive remote EEP. If a error occurs when PPU is in Run state, a Link error output then will be asserted by the PPU. Then the EEP may be written to the transmitter by the host(the user's application software). - "crc32_lib.v" on OC has been tailored to fit this pjt. It is optional. - Not like the Atmel's "TSS901E"(or called "SMCS332"),this ip core dosen't use a "clk10" but only a global clock "gclk".The "clk10" is not indispensable according to the SpaceWire standard and this may also be convenient. Note that not like TSS901E,the node channels doesn't support wormhole routing. All routing function is performed by Routers. ************** -ROUTER - bufferd switch - minimum switching latency and lowest propagation delay. - distributed scheduling, include output scheduling and the novel input scheduling( multi-RoutingTable). - ("sop_ack_o" is a sychrnous acknowledge signal indicate that the cell which a package want to be loaded has space to load. If it's true, after 1 clock, the controller will load data to that cell. --- now deleted) - Note if the buffer(eth_fifo) has data, the data emerges on the data output port currently is not valid. You need to read it (by a synchronous pulse) then the valid data occurs! The buffer is Revision 1.5 of "eth_fifo" which originally written by Igor Mohor from Slovenia. --------------------------------------------------- Limitations ----------------------------------------------------- - Function limitations: - - - +Conformity Limitations: |-- Link Interfaces --+ | |- +-- Router --+ |- TODO: the "Router" and various interface to other bus. ------------------------------------------ A little interesting topics ----------------------------------------------- 1) Open or close? In the "SpaceWire Router Requirements Specification(Issue:1 Rev: 5 Date:28.02.2003)" clause 4.1 has some words about this question: "Open VHDL Core The SpaceWire input/output ports shall be implemented with the Open VHDL core developed in the ESM006 contract for ESA [AD2]. Rationale: It will minimise design effort and help to validate the VHDL core." It did not refer to open the Router's IP,besides i have not found free "IO ports" core available on internet. 2) Georgia Institute of Technology introduced DX-Gt, a crossbar switch generator(generate Verilog code) for dynamic memory management in multiprocessor SoC in about 2003. 3) Active things:(observe at 03-26-2005) If someone has deep interest,you could pay attention to a conference "DASIA(DAta Systems In Aerospace) 2005" in Sheraton Grand Hotel, Edinburgh, Scotland during 30th May and 2nd June 2005. Tuesday 31st May 2005(SESSION 4B ON BOARD BUSES AND COMMUNICATION) [Chairperson: P. Plancke, ESA/ESTEC, The Netherlands] 09:00 Quality from SpaceWire and Quality into SpaceWire Systems B.M. Cook, P.H. Walker - 4Links, UK 09:30 SpaceWire Remote Memory Access Protocol S. Parkes, C. McClements - University of Dundee, UK 10:00 SpaceWire Internet Tunnel S. Mills, S. Parkes - University of Dundee, UK ------------------------------------------------ Annex ----------------------------------------------------------------- Annex A: Industry info and some Web site could be accessed for a further reference:: 1) "SpaceWire UK are specialist providers of VHDL Intellectual Property & Design Services for the Space Industry". The SpaceWire UK has developed a CODEC and SpaceWire Switch Core (Router) in VHDL for business. (I am sure i don't want to disturb this new ip vendor and I also had consulted their ip schemes.My try is just a hobby and want to contribute to promoting the SpW standard.) http://www.spacewire.co.uk 2) DSI GmbH is a German company which offers "SLI-Core", a VHDL CODEC Core for the SpaceWire Link Interface in June, 2004. Their English WEBs is preparing(observed in April,2005). http://www.dsi-it.de 3) The EADS Astrium GmbH (formed in May 2000 by the merger of Matra Marconi Space (France/UK) and the space division of DaimlerChrysler Aerospace (Germany)) is well known as the author of the "Router requirements spec" (Steve Parkes, University of Dundee). " ETD-031 'SpaceWire Router Development, Coordination and Validation' was Kicked-Off with Astrium the 2nd January 2002. " And the issue 1 rev 5 had been published on 28.02.2003. They described a router ASIC with internal configuration port,external pins for status/error monitoring (with status/error registers and control registers) in Feb,2004.It had been implemented in an Atmel MH1RT gate array. http://www.astrium.eads.net 4) Austrian Aerospace (AAE) has a switch ASIC, the Dynamic Switch Matrix (DSM), built in Atmel. " ESM-006 'SpaceWire Router ASIC development' is an ETD-031 sub-contract with Austrian Aerospace concerning the SpaceWire CODEC VHDL, router FPGA and router ASIC. " http://www.space.at 5) 4links derives from University of Dundee is a company that specializes in SpaceWire / IEEE1355 &Ethernet. They have some products such as EtherSpaceLink, SpaceWire-cPCI,SpaceWire-PCI,SpaceWire- Cables,and IPs which are relative to these products. They use Xilinx fpga implement routers with a performance well above 200 Mbit/s. http://www.4links.co.uk/index.htm 6) Webs of Chinese laboratory of avionics(for space use) say they are developing a SpW network system. http://www.spacee.net 7) Atmel offer SMCS332,SMCS Lite,and said their "potential future Standard ASICs & IPs include: SMCS Lite, SpaceWire Router(2004),SpaceWire Rx/Tx" in 2002. http://www.atmel.com 8) STAR-Dundee Ltd is a spin-out company of the University of Dundee set up specifically to support users of SpaceWire(fund from the Scottish Executive). Dr Steve Parkes was the Managing Director of STAR-Dundee, also the author of the SpaceWire standard document. "STAR-Dundee Ltd aims to fill the emerging market niche for research and development, debug and support tools for SpaceWire." But now STAR-Dundee Ltd offers many products like SpaceWire CompactPCI board,SpaceWire Router-USB for business. A few data sheets were published in March 24th,2005. Dr Steve Parkes: sparkes@@computing.dundee.ac.uk Press Officer: j.m.marra@@dundee.ac.uk http://www.star-dundee.com/ http://www.dundee.ac.uk 9) :--) Ask Google for more and fresh information. Annex B: Helpful reference for developers 1) I had tried to upload some HTMLs and PDFs to CVS but at the end i found that may be trying. Is it more laborsaving to just offer link info? And all developers must be happy to do that rather than uploading files from remote computers. 2) "Buffered Crossbar (CICQ) Switch Architecture", Computer Architecture & VLSI Laboratory, Institute of Computer Science,Foundation for Research and Technology, Hellas (FORTH) http://archvlsi.ics.forth.gr/bufXbar/ 3) Vinita Singhal, Robert Le: "High-Speed Bu ered Crossbar Switch Design Using Virtex-EM Devices", Xilinx Application Note 240 ; http://direct.xilinx.com/bvdocs/appnotes/xapp240.pdf 4) Xilinx Corporation:"Rocket IO Multi-Gigabit Tranceiver"; http://www.xilinx.com/products/virtex2pro/rocketio.htm 5) @ 1.3 log @a rough doc @ text @a1 1 /////////////////////////////////////////////////////////////// d3 2 d6 1 a6 2 "Spw grown organically from the needs of on-board processing applications. d10 3 a12 4 This Standard addresses the handling of payload data and control information on board a spacecraft. It is a standard for a high speed data link, which is intended to meet the needs of future, high capability, remote sensing instruments and other space missions. d14 3 a16 5 Processing units, mass-memory units and down-link telemetry systems developed for one mission can be readily used on another mission, reducing the cost of development, improving reliability and most importantly increasing the amount of scientific work that can be achieved within a limited budget. d18 2 a19 3 SpW is currently being installed on several NASA and European Space Agency (ESA) spaceships to support onboard communications during space missions.---27 January 2003) d21 1 a21 2 SpaceWire has taken into consideration two existing standards, IEEE 1355-1995 and ANSI/TIA/EIA-644. d23 3 a25 5 "Point-to-point serial links with LVDS. The maximum data signalling rate that can be achieved is different from one system to another, depending on several factors such as: 1)cable length, 2)driver-receiver technology, and 3)encoder-decoder design, and is limited by 4)skew and jitter." d31 5 d37 3 a39 11 Diff & Relation with IEE1355 device(eg. Atmel.Inc "TSS901E" which also called "SMCS332") "The SMCS devices implement revision A of the standard, which is based on IEEE1355. They do not implement the current version of SpaceWire. However, the current version of SpaceWire is backwards compatible with the earlier revision." ///////////////////////////////////////////////////////////////// d43 1 d46 1 a46 1 - CODEC d49 15 a63 9 - SWR - ...Synchronously Clocked Crosspoint...(Switch Latency...) - ... buffered crossbar...distributed scheduling(effective and simple). 16x16 now may be enough. * Due to the SpaceWire protocol,the file/module "SPW_CODEC.v" could be used as a core's top module (as a "channel") to be integrated with a "routing matrix" to form a router which is a Routing Switch in the SpaceWire network. Sometimes the CODEC is also called a "interface" or "input/output ports" of the router or a node device. See the scheme. * The file/module "SPW_I_vlogcore.v" is 3 CODEC with glue logic and Wishbone interface(COMI/HOCI) could be used as top module(a interface of the host to the SpW network) and be integrated into node devices. d65 11 a75 6 * The file/module "SWR_vlogcore.v" is a top module of Spacewire Router which integrates some interfaces and a Routing Matrix "SwitchCore.v" and a little other logic. This core is so rough now. * Had use some ip on the opencores.org such as a fifo(i have consulted the "plesiochronous_fifo.v" for the Receiver. For the transmitter which only need a synchronous fifo for internal usage,so i write a synfifo which was similar to Xilinx ip for less complexity.) and a CRC. * Note the LVDS driver and receiver is not contain in modules. * Triple Modulo Redundant (TMR). d83 1 d85 9 a93 1 A little specs: d99 3 a101 2 - The block "Receiver's clock recovery" in the scheme of the draft-1 is merged into the "Receiver". - The block "Transmitter clock generator" in the scheme of the draft-1 is merged into the "Transmitter". d106 12 a117 3 - The credit count keeped in "crd_cnt" which indicates the buffer space of the opposite Rx bufer is in the transmitter; at the same time the outstanding count keeped in "osd_cnt" which indicates the buffer data of the opposite Tx is in the receiver. - Notice that according to the custom of circuit operation,some name near the interface between the Tx/Rx and the fifo may be a little different from the standard document.(eg."TX_READY, TX_WRITE" may only present as a output pulse signal "rdbuf_o" to just read that mem. - Note that the Receiver do not generate local EEP to the host. It receive remote EEP, and if a error occurs when PPU is in Run state, a Link error output then will be asserted by the PPU. Then the EEP may be written to the transmitter by the host(the user's application software). a118 5 - Not like the Atmel's "TSS901E"(or called "SMCS332"),this ip core dosen't use a "clk10" but only a global clock "gclk".The "clk10" is not indispensable according to the SpaceWire standard and this may also be convenient. Note that not like TSS901E,the node channels doesn't support wormhole routing. All routing function is performed by Routers. d120 5 d126 1 d128 10 a137 7 - bufferd switch - ... minimum switching latency and lowest propagation delay ... - ... ... - ...operate directly on variable-size packets,...no packet segmentation and no scheduler(distributed scheduling decisions) - "sop_ack_o" is a sychrnous acknowledge signal indicate that the cell which a package want to be loaded has space to load. If it's true, after 1 clock, the controller will load data to that cell. - Note if the buffer has data, the data emerges on the data output port currently is not valid. You need to read it (by a synchronous pulse) then the valid data occurs! The buffer is Revision 1.5 of "eth_fifo" which originally written by Igor Mohor(from SI). d141 2 a142 1 ********************************************************* d148 1 a148 1 | |- d150 1 a150 1 |- a154 3 ************************************************************* ///////////////////////////////////////////////////////////////////////////////// d161 1 a161 2 Some interesting topics: d163 2 a164 2 In the "SpaceWire Router Requirements Specification(Issue:1 Rev: 5 Date:28.02.2003)" clause 4.1 has some words about this question: d166 2 a167 1 The SpaceWire input/output ports shall be implemented with the Open VHDL core developed in the ESM006 contract for ESA [AD2]. d169 2 a170 1 It did not refer to open the Router's IP,besides i have not found free "IO ports" core available on internet. d172 2 a173 1 2) Georgia Institute of Technology introduced DX-Gt, a crossbar switch generator(generate Verilog code) for dynamic memory management in multiprocessor SoC in about 2003. d176 3 a178 1 If someone has deep interest,you could pay attention to a conference "DASIA(DAta Systems In Aerospace) 2005" in Sheraton Grand Hotel, Edinburgh, Scotland during 30th May and 2nd June 2005. d194 1 a194 1 ////////////////////////////////////////////////////////////////////////////// a195 1 d198 5 a202 2 1) "SpaceWire UK are specialist providers of VHDL Intellectual Property & Design Services for the Space Industry". The SpaceWire UK has developed a CODEC and SpaceWire Switch Core (Router) in VHDL for business. (I am sure i don't want to disturb this new ip vendor and I also had consulted their ip schemes.My try is just a hobby and want to contribute to promoting the SpW standard.) d205 2 a206 1 2) DSI GmbH is a German company which offers "SLI-Core", a VHDL CODEC Core for the SpaceWire Link Interface in June, 2004. Their English WEBs is preparing(observed in April,2005). d209 8 a216 6 3) The EADS Astrium GmbH (formed in May 2000 by the merger of Matra Marconi Space (France/UK) and the space division of DaimlerChrysler Aerospace (Germany)) is well known as the author of the "Router requirements spec" (Steve Parkes, University of Dundee). " ETD-031 'SpaceWire Router Development, Coordination and Validation' was Kicked-Off with Astrium the 2nd January 2002. " And the issue 1 rev 5 had been published on 28.02.2003. They described a router ASIC with internal configuration port,external pins for status/error monitoring (with status/error registers and control registers) in Feb,2004.It had been implemented in an Atmel MH1RT gate array. d220 2 a221 2 " ESM-006 'SpaceWire Router ASIC development' is an ETD-031 sub-contract with Austrian Aerospace concerning the SpaceWire CODEC VHDL, router FPGA and router ASIC. " d224 5 a228 4 5) 4links derives from University of Dundee is a company that specializes in SpaceWire / IEEE1355 &Ethernet. They have some products such as EtherSpaceLink, SpaceWire-cPCI,SpaceWire-PCI,SpaceWire-Cables,and IPs which are relative to these products. They use Xilinx fpga implement routers with a performance well above 200 Mbit/s. d231 2 a232 1 6) Webs of Chinese laboratory of avionics(for space use) say they are developing a SpW network system. d235 2 a236 1 7) Atmel offer SMCS332,SMCS Lite,and said their "potential future Standard ASICs & IPs include:SMCS Lite, d240 6 a245 5 8) STAR-Dundee Ltd is a spin-out company of the University of Dundee set up specifically to support users of SpaceWire(fund from the Scottish Executive). Dr Steve Parkes was the Managing Director of STAR-Dundee, also the author of the SpaceWire standard document. "STAR-Dundee Ltd aims to fill the emerging market niche for research and development, debug and support tools for SpaceWire." But now STAR-Dundee Ltd offers many products like SpaceWire CompactPCI board,SpaceWire Router-USB for business. A few data sheets were published in March 24th,2005. d250 1 a250 1 http://star-dundee.com/ d254 17 a270 1 9) :--) Ask Google for more and fresh news. d272 3 d276 2 d279 3 @ 1.2 log @Add LSer, some tb @ text @d1 3 d5 15 a19 17 "Spw grown organically from the needs of on-board processing applications. (SpW is a network with Routers) This Standard addresses the handling of payload data and control information on board a spacecraft. It is a standard for a high speed data link, which is intended to meet the needs of future, high capability, remote sensing instruments and other space missions... Processing units, mass-memory units and down-link telemetry systems devel- oped for one mission can be readily used on another mission, reducing the cost of development, improving reliability and most importantly increasing the amount of scientific work that can be achieved within a limited budget. (SpW is currently being installed on several NASA and European Space Agency (ESA) spaceships to support onboard communications during space missions.---27 January 2003) SpaceWire has taken into consideration two existing standards, IEEE 1355-1995 and ANSI/TIA/EIA-644. "Point-to-point serial links with LVDS. The maximum data signalling rate that can be achieved is different from one system to another, depending on several factors such as: 1)cable length, 2)driver-receiver technology, and 3)encoder-decoder design, and is limited by 4)skew and jitter." d21 3 d25 2 d28 5 a35 3 Diff & Relation with IEE1355 device(eg. Atmel.Inc "TSS901E" which also called "SMCS332") "The SMCS devices implement revision A of the standard, which is based on IEEE1355. They do not implement the current version of SpaceWire. However, the current version of SpaceWire is backwards compatible with the earlier revision." d37 12 a48 1 ////////////////////////////////////////////////////////////////////////////////////// d58 1 a58 1 -SWR a104 4 d112 3 a114 1 d117 3 d140 1 a140 1 1)Open or close? d148 4 a151 3 2)Active things:(observe at 03-26-2005) If someone has deep interest,you could pay attention to a conference "DASIA(DAta Systems In Aerospace) 2005" in Sheraton Grand Hotel, Edinburgh, Scotland during 30th May and 2nd June 2005. d173 7 a179 8 The SpaceWire UK has developed a CODEC and SpaceWire Switch Core (Router) in VHDL for business. (I am sure i don't want to disturb this new ip vendor and I also had consulted their ip schemes.My try is just a hobby and have a heart to contribute to promoting the SpW standard.) www.spacewire.co.uk 2) The EADS Astrium GmbH (formed in May 2000 by the merger of Matra Marconi Space (France/UK) and the space division of DaimlerChrysler Aerospace (Germany)) is well known as the author of the "Router requirements spec" (Steve Parkes, University of Dundee). d185 1 a185 1 www.astrium.eads.net d187 1 a187 1 3) Austrian Aerospace (AAE) has a switch ASIC, the Dynamic Switch Matrix (DSM), built in Atmel. d190 1 a190 1 www.space.at d192 1 a192 1 4) 4links derives from University of Dundee is a company that specializes in SpaceWire / IEEE1355 &Ethernet. d196 1 a196 1 www.4links.co.uk/index.htm d198 2 a199 2 5) Webs of Chinese laboratory of avionics(for space use) say they are developing a SpW network system. www.spacee.net d201 1 a201 1 6) Atmel offer SMCS332,SMCS Lite,and said their "potential future Standard ASICs & IPs include:SMCS Lite, d203 1 a203 1 www.atmel.com d205 1 a205 1 7) STAR-Dundee Ltd is a spin-out company of the University of Dundee set up specifically to support users d209 1 d214 3 a216 6 www.dundee.ac.uk 8) Institute of Microelectronics, Micromechanics and Microoptics Hochschule Bremen ,University of Applied Sciences,Germany Spacewire interface (IP-Core) http://www.i3m.hs-bremen.de/internet/structure/elis/ d218 1 a218 1 9) :-> Ask Google for more and fresh news. @ 1.1 log @Initial revision @ text @d157 1 a157 1 2)The EADS Astrium GmbH (formed in May 2000 by the merger of Matra Marconi Space (France/UK) and the space division d167 1 a167 1 3)Austrian Aerospace (AAE) has a switch ASIC, the Dynamic Switch Matrix (DSM), built in Atmel. d172 1 a172 1 4)4links derives from University of Dundee is a company that specializes in SpaceWire / IEEE1355 &Ethernet. d178 1 a178 1 5)Webs of Chinese laboratory of avionics(for space use) say they are developing a SpW network system. d181 1 a181 1 6)Atmel offer SMCS332,SMCS Lite,and said their "potential future Standard ASICs & IPs include:SMCS Lite, d185 1 a185 1 7)STAR-Dundee Ltd is a spin-out company of the University of Dundee set up specifically to support users d195 6 a200 1 8) :--) Ask Google for more and fresh news. @ 1.1.1.1 log @no message @ text @@