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Title: COMPARATIVE SIMULATIVE ANALYSIS OF WDM LANS FOR AVIONICS PLATFORMS


1
COMPARATIVE SIMULATIVE ANALYSIS OF WDM LANS FOR
AVIONICS PLATFORMS
  • Casey B. Reardon, John D. Profumo,
  • and Alan D. George
  • HCS Research Laboratory
  • University of Florida

2
Outline
  • Introduction
  • Modeling Overview
  • Proposed Network Architectures
  • Ring-Ring
  • Optical Trees
  • Switched Hybrid
  • Optically Switched Clos
  • Experimental Setups
  • Platform Configurations
  • Simulation Parameters
  • Results
  • Latency Statistics
  • Analysis of Results
  • Conclusions

3
Introduction
  • Optical network technology for avionics is
    rapidly maturing
  • Increased reliability, performance,
    cost-effectiveness of optical components
  • Emergence of optical switch technology offers
    further augments to performance, flexibility and
    scalability to WDM networks
  • Desire for unified backbone local-area network
    (LAN) on avionics platforms
  • Provide universal network for all avionics
    devices to simplify design, wiring, and increase
    scalability
  • Introduces a challenge to provide packet-switched
    LAN performance using connection-based components
  • WDM an attractive option for next-generation
    avionics network
  • Huge bandwidth capacities, better weight
    characteristics, protocol transparency, etc.
  • First phase of on-going research project to
    design and evaluate WDM avionics architecture
    designs via virtual prototyping

4
Modeling Overview
  • MLDesigner selected as simulation modeling tool
  • Discrete-event simulation environment, developed
    by MLDesign Technologies Inc.
  • Advantages offered by MLD
  • Models are fully extendible and user-definable
  • Inherent hierarchical design facilitates modeling
    at multiple levels
  • LION Library for Integrated Optical Networking
    1
  • Bridge gap between optic-centric and
    network-centric modeling and simulation analysis
    tools
  • LION currently contains 39 optical component
    modules
  • Components include couplers, splitters, lasers,
    receivers, etc.
  • Parameters model key timing and physical
    component effects
  • Low-level components used to realize any number
    of higher-level modules

Example Optical Receiver Model in LION
5
Proposed Architectures and Requirements
  • Requirements of the WDM avionics LAN
  • Support up to 256 nodes
  • High-speed, deterministic communication between
    any two nodes
  • Easy implementation on contemporary platforms
    with fewer nodes
  • Detection and recovery from one or two faults,
    graceful degradation after three faults
  • To design and identify an ideal WDM avionics LAN
    architecture to meet above requirements, numerous
    disparate approaches need to be evaluated
  • Candidate designs represent examples of optical
    network architectures developed for alternate
    networking applications
  • Six candidate architectures proposed, modeled,
    and evaluated in this study
  • Ring-ring
  • Optical tree
  • Both with TDMA and RSVP control protocols
  • OSMOSIS-based Optical Clos
  • Matisse-based Hybrid

6
Ring-Ring Architecture
  • Based off proposed ROBUS architecture design 2
  • Nodes connected among several local rings
  • Up to 16 nodes per ring
  • Local rings connected by a central master ring
  • Dual-fiber rings allow operation in presence of
    fiber cut(s)
  • Ring-leader node provides inter-face between
    local master ring
  • Two control protocols used with this topology
  • Each destination on local rings assigned one
    wavelength for both protocols
  • Wavelengths re-used among rings
  • TDMA protocol, static timeslots assigned to each
    transmitter
  • RSVP protocol, control wavelength used to
    schedule transmissions, ring-leader grants
    requests
  • Inter-ring traffic buffered at ring-leader of
    destination for both protocols

Ring-Ring Architecture Diagram
7
Optical Tree Network
  • Nodes connected to one of several local trees 3
  • Up to 16 nodes per tree
  • Local trees connected by a central coupler
  • Dual-fiber rings allow operation in presence of
    fiber cuts
  • Tree-leader node provides interface between local
    trees
  • Two control protocols used with this topology
  • Each destination on local trees assigned one
    wavelength
  • Wavelengths re-used among trees
  • TDMA protocol, static timeslots assigned to each
    transmitter
  • RSVP protocol, control wavelength used to
    schedule transmissions, tree-leader grants
    requests
  • Inter-tree traffic buffered at tree-leader of
    destination for both protocols

Optical Tree Architecture Diagram
8
Optic-Electro Switched Hybrid
  • Example of a optical-electrical hybrid network
  • Network consists of COTS Ethernet switches,
    inter-connected with a WDM ring
  • 32-port Ethernet switches, all w/ electronic GigE
    links
  • Optical receiver arrays allow for a dedicated
    wavelength between each pair of switches
  • Central memory switching models, w/ QoS disabled
  • Nodes interface with avionicsEthernet NICs
  • Use of Ethernet componentsmakes network
    cost-efficient
  • Network design based largelyoff commercial
    solutions, e.g. Matisse Networks 5

Hybrid Architecture Diagram
9
OSMOSIS Clos Network
  • Optical-switch Clos network using OSMOSIS-based
    modules 4
  • Each connection includes both an optical and
    electronic link
  • Optical path used for data transmission
  • Electronic path used to request and reserve
    optical paths
  • Transmission requests are made to the switch
    arbiter, which services requests in round-robin
    format
  • Data transmissions broken up into timeslots
  • Senders are granted a number of timeslots for
    data transmission by the arbiter
  • Broadcast-and-select optical switching, allows
    each output to select any input optical signal
  • 100 ns of each timeslot reserved to perform
    optical switching w/ SOAs
  • Network connected in Clos topology 7
  • Nodes connected to one of eight 32-node
    perimeter switches
  • Each perimeter switch connected to three
    backbone switches
  • Inter-switch traffic buffered at intermediate
    switches

Optical Clos Architecture Diagram
10
Experimental Configurations
  • Federated Commercial Platform
  • Based off avionics network traffic data provided
    by Rockwell Collins Inc.
  • Processing and communication distributed among
    subsystems
  • Commercial Platform Layout
  • 86 Nodes, in 8 subsystems
  • 300 Mbps baseline traffic

Commercial Configuration Diagram
  • Centralized Military Platform
  • Based off of the F-22 Raptor platform 6
  • Most processing, inter-system traffic flows
    through Core Processing (CP)
  • Military Platform Layout
  • 97 Nodes, in 7 subsystems
  • 200 Mbps baseline traffic

Military Configuration Diagram
11
Simulation Parameters
  • Four simulative experiments run for each system
  • Commercial and military configurations
  • Baseline and 10x traffic rates
  • Global simulation constants
  • All optical transmitters and receivers operate at
    2.5 Gbps, per wavelength
  • Results accumulated for 1 second of network
    traffic
  • 1 µs tuning delay in tunable lasers and receivers
  • Message sizes uniformly distributed between 100
    and 2,500 bytes
  • Architecture-specific simulation parameters
  • 1 Gbps electronic link speed used with Clos and
    Hybrid architectures
  • 500 ns OSMOSIS switch timeslot used in the Clos
    architecture
  • Timeslot periods in both TDMA architectures were
    500 µs for local traffic and 600 µs for traffic
    between rings or trees
  • Reported Results
  • Average packet latency for entire system
  • Average worst-case packet latency the average of
    the 10 highest packet latencies in the system

12
Results - Summaries
Table 1 Summary of Overall Packet Latency (us)
Table 2 Average Worst-case Packet Latency (us)
13
Analysis of Results
  • Clos network exhibits the highest performance in
    all four experiments
  • Average latency twice as fast as the next best
    network, due to high bandwidth in switches and
    fast parallel scheduling techniques
  • Average latencies constant in the 20-25 us range
    in all cases, showing excellent scalability
    capabilities
  • Easy to support additional nodes by adding
    switches to perimeter
  • High-performance of Clos network comes at a price
  • Clos networks are highly connected, leading to
    complex wiring demands
  • Optical switch components are unproven for use in
    avionics
  • Fault-tolerance requires redundant switches at
    each perimeter location

Average Latency (Baseline Military)
14
Analysis of Results
  • Hybrid network exhibited second-best performance
    throughout experiments
  • Latencies twice as slow as Clos, but orders of
    magnitude faster than ring and tree networks
  • Electronic switching does not waste bandwidth,
    and allows flexibility for network to handle
    traffic bursts
  • Low-cost of deployment another key advantage for
    architecture
  • Performance dropped as traffic scaled, especially
    on military platform
  • Limited switch bandwidth compared to optical
    switches
  • High contention levels created on core
    processings switch
  • Use of smaller switch modules and AFDX techniques
    could relieve strain on individual switches, add
    deterministic behavior

Average Latency (Baseline Commercial)
15
Analysis of Results
  • Little variation observed between ring-ring and
    tree architectures
  • Fault-tolerance of rings outweighs minimal
    performance gains of trees resulting from their
    fixed-length lightpaths
  • Both RSVP architectures fared far better than
    TDMA architectures
  • Observed average latencies of 140 and 230 µs in
    baseline experiments
  • RSVP suffers in scenarios with several sources
    sending to one destination
  • The slow method of optical arbitration causes
    significant delays when multiple bursts need to
    be sent to the same node
  • A faster, parallel arbitration method would
    greatly increase the performance potential of the
    RSVP architectures
  • Average and worst-case latencies saw large
    increases in 10x experiments
  • Poor scalability of RSVP causes increases need
    for faster arbitration
  • Available bandwidth for data transmission is not
    currently the major bottleneck
  • Additional mechanisms necessary to increase
    determinism of RSVP protocol, as evidenced by
    observed worst-case latencies
  • TDMA offered the slowest performance of all
    architectures
  • Latency increased super-linearly as traffic rates
    scaled
  • Worst-case latencies exceeded 1 second in 10x
    experiments
  • TDMA not equipped to efficiently handle traffic
    bursts
  • As the node count increases, the fraction of
    bandwidth available to each node decreases
  • Alternate TDMA techniques likely would not
    improve performance by multiple orders of
    magnitude, thus pure TDMA does not appear to be a
    viable control protocol to serve an avionics LAN
    with a large number of nodes

16
Conclusions
  • Much insight gained from evaluation of several
    WDM architectures for avionics platforms
  • Purely passive approaches do not offer optimal
    performance
  • Dynamically establishing lightpaths on shared
    optical mediums with purely optical networks led
    to inefficient and disappointing performances
  • Highly intelligent and efficient control
    protocols required for passive buses, rings or
    trees to serve a large number of nodes
    effectively
  • Switched networks with buffering and fast
    scheduling capabilities exhibit superior
    performance
  • Such networks have also proven effective for
    networks of varying scales
  • Key tradeoffs between performance, reliability
    and ease of implementation need to be considered
  • While optically switched networks may offer
    highest performance, reliability and wiring
    complexity need to be addressed
  • Clos leads to complex wiring demands, and
    numerous redundant switches required to prevent
    single-point of failures
  • Ring-based architectures provide inherent
    fault-tolerance
  • An approach combining the benefits of electrical
    and optical technologies may lead to ideal
    avionics network solution
  • Leverage the strengths of both optical and
    electronic technologies

17
Future Work and Acknowledgements
  • Future Work
  • Study and evaluation of additional WDM
    architecture designs
  • Consideration of alternate optical switching
    architectures, higher number of control protocol
    combinations
  • Sensitivity analyses of variable parameters
    within each architecture
  • e.g. timeslot periods, non-static timeslot
    allocations, varying switch port counts,
    available wavelengths, non-fixed wavelength
    allocations, etc.
  • Investigate mechanisms for providing
    connection-oriented services
  • e.g. pre-allocation of resources for periodic
    transmissions
  • Consideration of multicast traffic in simulative
    experiments
  • Incorporate legacy network protocols into
    experimental configurations
  • e.g. MIL-STD-1553, AFDX, ARINC 429, etc.
  • All investigated candidates and options to
    support SAEs avionics WDM LAN standard
    development
  • Acknowledgement
  • This work was made possible by Navy STTR WDM
    Fiber-Optic Network Architecture Analysis,
    Modeling, Optimization, and Demonstration for
    Aerospace Platforms (c/o NAVAIR)

18
References
  • 1 C. Reardon, I. Troxel and A. George, "Virtual
    Prototyping of WDM Avionics Networks," Proc. of
    Avionics Fiber-Optics and Photonics (AVFOP)
    Conference, MIT Lincoln Lab, Minneapolis, MN,
    Sep. 20-22, 2005.
  • 2 Gardner, R., et al., High-Performance
    Photonic Avionics Networking Using WDM, MILCOM
    1999, Volume 2, 31 Oct.- 3 Nov. 1999, pp.
    958-962.
  • 3 Gerla, M., Kova, M., and Bannister, J.,
    Optical Tree Topologies Access Control and
    Wavelength Assignment, Computer Networks and
    ISDN Systems Journal, Vol. 26, No. 6-8, pp.
    965-983, 1994.
  • 4 Hemenway, R., and Grzybowski, R.,
    Optical-Packet-Switched Interconnect for
    Supercomputer Applications, Journal of Optical
    Networking, Vol. 3, No. 12, pp. 900, Dec. 2004.
  • 5 Matisse Networks, www.matissenetworks.com.
  • 6 Spitzer, Carl, The Avionics Handbook, CRC
    Press LLC, Boca Raton, Florida, 2001.
  • 7 Clos, Charles, A Study of Non-Blocking
    Switching Networks, Bell System Technical
    Journal, March 1953, pp.406-424.
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