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Tommy Baumann, David Hipkins, John Mester

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The Gravity Probe B Relativity Mission W.W.Hansen Experimental Physics ... of Aeronautics & Astronautics 50th Anniversary Symposium & Celebration May 8 ... – PowerPoint PPT presentation

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Title: Tommy Baumann, David Hipkins, John Mester


1
Model Based Design, Analysis and Validation of
STEP using MLDesigner and SatLab
  • Tommy Baumann, David Hipkins, John Mester

The System Design Tool MLDesigner
Extended Mission Level Design Flow
Specification of STEP
  • Efficiency of tools grows maximum 25 per year
    while complexity of electronic systems grows 65
    per year? System Design Gap
  • Increasing abstraction widens discrepancy between
    design and implementation ? System
    Abstraction Gap
  • Finding appropriate design regarding increasing
    count and complexity of requirements? Design
    Space Exploration
  • Improving quality and speed of specification
  • Is the leading modeling and simulation tool for
    design of networked systems
  • Automates the design process from mission
    requirements to implementation handoff
  • Is a multi-domain simulator, that combines
    modeling and simulation capabilities found in
    various design tools
  • Although MLDesigner supports bottom-up design, it
    is designed for top-down design, iterative design
    process (sometimes called a spiral design process)
  • Design of an executable, model based
    specification of STEP
  • Common description of environment, function and
    architecture
  • Multi-domain approach (CTDE, DE, SDF, FSM)
  • Figure Architecture/ Performance Level (DE)
  • Design of Payload and Service module
  • Integration of PCI and 1553 protocols

F1
P2
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System
F2
F3
P1
P1
F4
P2
P1
Module
F5
F7
F6
P1
P2
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F8
P3
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P7
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P5
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State Machine
Primitive
Module
  • Black box principle
  • Hierarchical decomposition
  • Domain combination
  • Reusable model elements
  • Figure Function and Mission Level (DE)
  • Connection of MLDesigner SatLab
  • Usage of satellite orbit information(position
    andangular velocity)
  • Discretization of continuous dataand vice versa
  • Control loop interface

The Satellite Environment Tool SatLab
  • Is a tool for mission and system level design,
    animation, and analysis of mobile/satellite
    communication and navigation systems
  • Provides a simulation engine with the fast
    orbital propagator and trajectory generator for
    mobiles (aircrafts, missiles, cars, etc..)
  • Provides an animation system with views from
    space, from earth and in 3D terrain, coverage
    analysis, circle views and path loss view in 3D
    terrain
  • Contains a terrain data base system, compatible
    with USGS DEM, USGS Land Usage data, and DMA DTED
    data
  • Contains the high-level programming language
    SatLab Command Language (SCL)
  • Figure Functional Level (CTDE)
  • Abstraction of physical proof mass behaviour
  • Design of differential equations in form of
    block diagrams
  • Output of proof mass position
  • Influenced by satellite and control
  • Satellites with either circular or elliptical
    orbits
  • Fixed earth stations at any latitude, longitude
    and altitude
  • Mobile earth stations
  • Parameters to define all system parameter values
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