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RunTime Behavior of Ardea: A Dynamically Reconfigurable Distributed Embedded Control Architecture

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preemptive, real-time, multi-tasking, priority-based kernel. ... Stock Flight Systems. NASA Langley AGATE/SATS ... Tracking resource availability (HW and SW) ... – PowerPoint PPT presentation

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Title: RunTime Behavior of Ardea: A Dynamically Reconfigurable Distributed Embedded Control Architecture


1
Run-Time Behavior of Ardea A Dynamically
Reconfigurable Distributed Embedded Control
Architecture
  • Osamah A. Rawashdeh and James E. Lumpp, Jr.
  • Department of Electrical and Computer Engineering
  • University of Kentucky
  • Lexington, KY

2
Outline
  • Motivation/Background
  • Objective and Contributions
  • Ardea Framework Overview
  • Ardea Hardware Architecture
  • Software Module Dependency Graphs
  • Ardea Fault Tolerance
  • Runtime Behavior
  • Summary and Conclusion

3
Embedded Control
  • Distributed embedded control system
  • Mission critical tasks
  • Non-mission critical tasks
  • Array of sensors and actuators
  • Set of computing resources
  • Interconnection network

4
Distributed Fault-Tolerance
  • Nodes, links and software can fail
  • Fault tolerance entails fault detection/handling
  • Requires redundancy
  • Static redundancy (spatial redundancy)
  • Modular redundancy
  • Design Diversity
  • Dynamic redundancy (temporal redundancy)
  • Recovery blocks
  • Failover programming
  • Roll-back/roll-forward
  • Real-Time deadlines

5
BIG BLUE
  • BIG BLUE Baseline Inflatable-wing Glider,
    Balloon- Launched Unmanned Experiment.
  • Ongoing project at UK to developing a test bed
    for Mars airplane technology.
  • 40 undergraduate students involved per year.

6
UAV Research
  • BIG BLUE is funded by NASA Workforce Development
    Program.
  • Dependable UAVs for Homeland Security
  • BIG BLUE III, with inflatable only wings, and a
    UAV for entry in the AUVSI 3rd Annual Student UAV
    Competition.
  • READY UAV

7
BIG BLUE II Architecture
  • Mission Controller
  • Auto-Sequencing
  • Data Acquisition
  • Ground Communication
  • Flight Controller
  • Control Glider
  • Chute Control
  • Monitor System Status
  • Deploy Recovery Chute
  • Camera Driver
  • Capture Images
  • Store to NVRAM
  • Shared Memory Space
  • Mailbox-Based Messaging

8
Reconfiguration Based FT
  • Run-time reconfiguration feasible in distribute
    embedded systems
  • Cost, size, power constraints
  • Availability of non-critical resources
  • Graceful degradation a loss of or reduction in
    the quality of services a system provides in
    response to faults

9
Approach
  • Hardware/Software faults degrade performance
    instead of causing system failure.
  • Resources dedicated to non-critical functions
    serve as backup resources for critical functions.
  • No need to consider every failure combination at
    design time.
  • Objective To develop a framework for specifying
    gracefully degrading distributed embedded systems.

10
Primary Challenges
  • Specify static and dynamic redundancies as well
    as graceful degradation
  • Provide Run-time infrastructure for these
    applications

11
The Ardea Framework
  • Ardea Automatically Reconfigurable Distributed
    Embedded Architectures
  • Ardea herodias The Great Blue Heron, a wading
    bird of the heron family Ardeidae, common all
    over North and Central America. This is the
    largest North American heron.

12
HW Architecture Overview
  • Processing Elements (PEs)
  • - Homogeneous set of processors
  • - Real-time OS.
  • - Local management tasks (scheduler,
    network interface, loader)
  • I/O Devices
  • - Sensors and actuators
  • - Hosted by PEs
  • Communication Network
  • - Broadcast Network
  • - Bandwidth and Latency
  • System Manager
  • - Fault tolerant by other means
  • - Tracks status of resources
  • - Finds and deploys configurations

13
Micro C/OS-II
  • Portable, ROMable, scalable,
  • preemptive, real-time, multi-tasking,
    priority-based kernel.
  • Source available, ANSI C and free for academic
    use.
  • Ported to 40 architectures (8 to 64 bit) since
    1992.
  • Meets RTCA DO-178B Level 1
  • Uses 4 CPU and 3 KB - 30 KB RAM

14
CAN Aerospace
  • Stock Flight Systems
  • NASA Langley AGATE/SATS
  • NASA Ames SOFIA

15
Specifying Fault Tolerance
  • Specifying static redundancy
  • Modular redundancy
  • N-version programming
  • Specifying dynamic fault redundancy
  • Roll-back
  • Roll-forward
  • Specifying graceful degradation
  • Multi-version software modules
  • Shedding non-critical services
  • Reducing update/output rate of services

16
Application Specification
  • Dependency graphs show the periodic flow of
    information from sensors to actuators (i.e., data
    pipelines)
  • Graph nodes software modules, data variables,
    I/O devices, and dependency gates
  • Software modules
  • Executable code schedulable
  • on a processing element
  • Suspended while input(s) unavailable
  • Produce and consume data variables
  • Attributes worst case execution time
  • and rate factor

17
Data Flow
  • Data variables
  • Application data between
  • software modules
  • State data variables are local to a software
    module
  • Management data variables contain data consumed
    by system manager.
  • Attributes
  • Size
  • Quality value or function

Figure 5 - Page 19
18
Specifying Dependencies
  • Dependency gates
  • k-out-of-n OR gates n gt 0,
  • 0 k n
  • AND all input required
  • XOR only one input required
  • DEMUX for fanning out
  • OR gates can be specified to distribute inputs

19
Node Attributes
ID yaw_cntrl1 Exec_T 900 cycl. Rate_factor
15
ID out1, out2 Criticality critical Priority
1, Rate 10 Hz State Enabled
ID rud_Angle1 Size 2 bytes Quality 1
ID mag_drv1 , mag_drv2 Exec_T 300
cycl. Rate_factor n/a
ID yaw_history Size 8 bytes Quality n/a
ID servo1_drv, servo2_drv Exec_T 200
cycles Rate_factor 11
ID yaw1, yaw2 Size 2 bytes Quality 1, 2
ID rud_Angle2 Size 2 bytes Quality 2
ID yaw_cntrl2 Exec_T 400 cycl. Rate_factor
12
20
Ardea Fault Detection Handling
  • Failure detection of sensors, actuators and
    software modules is the responsibility of
    application software
  • Ardea built-in fault detection
  • PE crash failures by heartbeat messages
  • Network link failures detected and handled as PE
    failures
  • Software module crashes detected locally by a
    module execution monitors
  • Critical output modules detect missed deadlines
  • Fault Handling masking, reconfiguration, or
    fail-stop

21
Sensor Fault Detection
22
Actuator Fault Detection
23
Software Fault Detection
24
Triple Modular Redundancy
25
The Challenges
  • Software mode location independence
  • Moving object code
  • Routing module I/O data
  • Fault Recognition
  • User/application code reported faults
  • Ardea built-in fault detection
  • Tracking status/availability of HW and SW
    resources
  • Configuration Management
  • Tracking resource availability (HW and SW)
  • Finding new configurations (mapping of modules to
    PEs)
  • Deploying new configurations (starting, stopping,
    and restarting modules)
  • Managing state data variables
  • Reconfiguration time and critical deadlines.
    (multiple system reconfiguration policies to
    support reconfiguration before deadlines are
    missed. If a deadline is missed, then system
    fail-stop)

26
The System Manager
27
Processing Elements (PEs)
  • Memory Loader copies code into program memory
  • Scheduler starts and stops execution of modules
  • Network Interface handles public data variables
    (data routing)

28
Scheduling and Unscheduling
  • Starting, stopping, and restarting modules
  • Restarting requires
  • State Preservation
  • Unprocessed data preservation

29
Reconfiguration Policies
  • Two configuration finding algorithms
  • High-fidelity is (NP-hard) to find high-utility
    configurations
  • Low-fidelity (fast) to insure running of critical
    services
  • Response based on criticality of
    detected/reported fault
  • Deploying configurations starting from sensor
    side of a DG

30
Reconfiguration Policies
31
Ardea Features
  • Ardea provides a structured framework for the
    design and implementation of real-time systems
  • Dependency graphs for application software
    specification
  • Run-time support for portable software modules,
    fault recognition, and handling
  • More flexible fault-tolerance at reduced cost
  • Specify reconfigurable systems using DGs
  • Simplified debugging and maintenanc
  • Graceful upgrade and repair
  • Software reusability

32
Current Work
  • Applying techniques to a UAVs student UAV
    competitions.
  • Avionics system for BIG BLUE Mars Airplane.
  • READY UAV Project
  • Expand bus via wireless link
  • Rapid prototyping
  • Minimize risk to hardware
  • Flexible Reconfiguration
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