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1 The SpaceWire Internet Tunnel and the Advantages It Provides For Spacecraft Integration Stuart Mills, Steve Parkes Space Technology Centre University.

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Presentation on theme: "1 The SpaceWire Internet Tunnel and the Advantages It Provides For Spacecraft Integration Stuart Mills, Steve Parkes Space Technology Centre University."— Presentation transcript:

1 1 The SpaceWire Internet Tunnel and the Advantages It Provides For Spacecraft Integration Stuart Mills, Steve Parkes Space Technology Centre University of Dundee Raffaele Vitulli ESA, ESTEC

2 2 Introduction  Spacecraft Integration  The SpaceWire Internet Tunnel  Technical Difficulties and Overcoming Them  The SpaceWire Internet Tunnel Server  The TopNet Pilot Study  Advantages of the Tunnel  Summary and Conclusions

3 Spacecraft Integration 3

4 Normal Integration Procedures  Integration Testing performed late in development process –Problems expensive to correct  Problem of geographical separation  Importance of interface specifications  Advantages of standard interfaces –SpaceWire  Problems still possible at higher layers –Application level 4

5 Virtual Spacecraft Integration  Remote sub-systems connected using the Internet  Integration testing can be performed without bringing components to one physical location  Reduces travel  Problems can be identified in interface specifications and implementations  Integration can be performed earlier in the development process 5

6 The SpaceWire Internet Tunnel 6

7 SpaceWire Internet Tunnel  Developed by the University of Dundee under ESA contract  Now a commercial product available from STAR-Dundee  A Tunnel replaces a SpaceWire link with a connection over a network –Such as the Internet  Hardware and software solution  Protocol Analysis software also provided –Monitor the Tunnelled traffic 7

8 Example Network with Two Sub-Systems 8 Mass Memory Unit Processor Router Camera Instrument 1 Camera Instrument 2 Router SpaceWire Sub-System 1 SpaceWire Sub-System 2

9 Example Network with Tunnel 9 Internet Mass Memory Unit Processor Router Camera Instrument 1 Camera Instrument 2 Router SpaceWire Sub-System 1 SpaceWire Sub-System 2 SpaceWire IP-Tunnel PC running SpaceWire IP Tunnel Software SpaceWire IP-Tunnel PC running SpaceWire IP Tunnel Software

10 SpaceWire Internet Tunnel  Transparently replaces a SpaceWire link  Traffic entering the Tunnel will exit in the same order –A time-code will be between the same two data characters  Link start and disconnect are also represented  Only difference is in bandwidth and latency –Limitations of Internet 10

11 SpaceWire Internet Tunnel Hardware  Connects to a PC using USB  Provides two SpaceWire links –Can create two Tunnels per device 11

12 SpaceWire Internet Tunnel Software  Runs on Windows and Linux –Java software so doesn’t need recompiled for each platform –Dependant on hardware drivers  Secure connection used to ensure traffic cannot be viewed or modified –A password can also be specified for each Tunnel  Mechanisms provided to cope with bandwidth and latency limitations of the Internet –To avoid timeouts at routers 12

13 SpaceWire Protocol Analyser Software  Protocol Analysis software built in to the SpaceWire Tunnel Software  Allows traffic crossing the Tunnel to be monitored and recorded  Traffic statistics can be viewed in real time  Higher Layer Protocol Plug-Ins can be added –Allows the properties of any protocol to be monitored and recorded –RMAP packets or an application specific protocol –Can be written by users –Loaded at run-time 13

14 SpaceWire Internet Tunnel Software 14

15 Technical Difficulties and Overcoming Them 15

16 Potential Limitations Identified  Issues relating to bandwidth and latency restrictions of the Internet  Security concerns related to sending data across the Internet  Problems establishing connections over the Internet 16

17 Bandwidth and Latency Restrictions  Gaps in packets can cause SpaceWire routers to timeout  Mechanisms provided in Tunnel to avoid these timeouts –Present in both the Tunnel entrance and exit  Still some systems where a Tunnel is not appropriate –Packets expected within a restricted time period –High bandwidth 17

18 Security Concerns  All traffic sent using Transport Layer Security (TLS)‏ –Same mechanism used by secure websites –All traffic encrypted –Cannot be viewed or modified  Password used to ensure the other end is who they claim to be –Also sent encrypted using TLS 18

19 Problems Establishing Connections  Proxy server issues  Firewall restrictions  Client-server limitations –Firewall restrictions need to be relaxed at the server side of a Tunnel connection  Support for proxy servers added to software  Software allows any TCP port to be used –Using the port assigned for TLS web traffic can get Tunnel traffic through intelligent firewalls  Tunnel Server Software developed… 19

20 The SpaceWire Internet Tunnel Server 20

21 SpaceWire Tunnel Server  Internet communication uses a client-server model  This requires one end to act as a server –Normally requires special firewall permissions –Many organisations will not allow this  Some users can only act as the client in a Tunnel connection –Can only connect to users in organisations which have the necessary firewall permissions to act as the server 21

22 SpaceWire Tunnel Server  Allows two PCs running the SpaceWire Internet Tunnel Software to connect  Neither PC must act as a server –Both are clients  Routes data from one client to the other  Avoids firewall restrictions –Any PC can operate as a client –Only the Tunnel Server PC has to have special firewall permissions  Makes testing of multiple sub-systems simpler –Users do not have to know the address of each client they are connecting to, only the server’s address 22

23 SpaceWire Tunnel Server  Capable of managing multiple client pairs  A single Tunnel Server could manage connections from multiple organisations  Alternatively an organisation could run their own Tunnel Server to manage all their connections 23

24 SpaceWire Tunnel Server  Restrictions can be applied to connecting clients based on –IP address –TCP port –Password  Uses same secure connections as SpaceWire Tunnel Software (TLS)‏  Completely transparent to the clients running the Tunnel Software –Has no effect on the mechanisms used to cope with bandwidth and latency restrictions 24

25 SpaceWire Tunnel Server Software  Runs on all platforms which support Java –Java software so doesn’t need recompiled for each platform –Doesn’t use any hardware, so not dependant on hardware drivers  Distributed with the Tunnel software and hardware 25

26 The TopNet Pilot Study 26

27 TopNet Pilot Study  ESA pilot study to investigate benefits and limitations of virtual spacecraft integration and the SpaceWire Internet Tunnel  A number of organisations in several countries involved  Performed experiments, integrated components virtually using the Tunnel  Reported back on their results and experiences 27

28 TopNet Pilot Study  Summary of findings: –Virtual spacecraft integration and the SpaceWire Internet Tunnel can be very useful for integration testing –Still improvements that can be made  Feedback from pilot contractors has lead to improvements to the Tunnel software and hardware –Some improvements made during study –Others have been made following final presentations 28

29 Advantages of the Tunnel 29

30 Advantages of Virtual Spacecraft Integration  Earlier integration –Identify and correct problems earlier –Saves time and money as easier to correct problems identified at an earlier stage  Less travel –With associated financial and environmental savings  Improved flexibility –Integration testing can be performed at any time –Sub-systems can easily be replaced by simulations  Improved cooperation –Allows multiple organisations (or a single organisation with multiple sites) to work on the same system 30

31 Potential Limitations of Virtual Spacecraft Integration  Potential limitations identified earlier: –Bandwidth and latency restrictions of the Internet –Security concerns –Connection establishment problems 31

32 Advantages of the SpaceWire Tunnel  Provides all the benefits of virtual spacecraft integration  Addresses most of the limitations 32

33 Features of the SpaceWire Tunnel  Bandwidth and Latency Restrictions –Software provides mechanisms to cope with poorer and varying bandwidth and latency –But still some SpaceWire systems where the Tunnel is not suitable  E.g. a camera which expects to continually send images at a high rate and expects the SpaceWire link to never be blocked –Pilot users found that it was often possible to perform limited integration testing for such systems –Some suggested the addition of specific software and hardware modes to a system under test to allow virtual integration testing  E.g. with relaxed timing requirements 33

34 Features of the SpaceWire Tunnel  Security –All traffic sent over a Tunnel is encrypted using TLS/SSL –A password for the Tunnel can be specified –A password can also be specified for the Tunnel Server  Connection Establishment Issues –Software allows any TCP port to be used  Using an appropriate port, a firewall will see the traffic as no different to a secure web page –Use of a Tunnel Server avoids the client-server limitations on the end users 34

35 Features of the SpaceWire Tunnel  Other issues from the Pilot Study –Many improvements suggested to the Protocol Analysis software  Highlighted the importance of analysis tools when performing integration testing  Additional advantages identified –Virtual integration testing can take a fraction of the time of full integration testing –Not necessary to transport EGSE to an integration site –Some users now use the Protocol Analyser software to monitor SpaceWire traffic  Without actually Tunnelling 35

36 Summary and Conclusions 36

37  Tunnel has been successfully demonstrated across Europe  The benefits of virtual spacecraft integration and the SpaceWire Internet Tunnel are clear  Recent improvements to the SpaceWire Tunnel and the addition of the SpaceWire Tunnel Server increase these benefits  Feedback from Pilot activity –Validated concept and implementation –Allowed improvements to be made 37

38 Summary and Conclusions  TopNet Pilot Study has shown that virtual spacecraft integration can be used in real projects  Although physical integration testing is still essential, virtual integration testing can be an important and beneficial stage in future projects 38


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