Low cost, minimal complexity and rapidly prototyped "common bus" design


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Lunar Atmosphere and Dust Environment Explorer (LADEE) is a NASA mission that will orbit the Moon and its main objective is to characterize the atmosphere and lunar dust environment.

  • Lunar Atmosphere and Dust Environment Explorer (LADEE) is a NASA mission that will orbit the Moon and its main objective is to characterize the atmosphere and lunar dust environment.

    • Low cost, minimal complexity and rapidly prototyped “common bus” design.
    • Model-Based Software Development


  • Review of LADEE Development Process & Software Architecture

  • Some Lessons Learned

  • Model Based Development

  • NPRs/CMMI

  • Model Based Development

  • “Just In Time” organizations

  • Interface Control Documentation

  • Emergent Behavior

  • Current Status



Development Approach

  • Development Approach

    • Model Based Development Paradigm (prototyped process using a “Hover Test Vehicle”)
    • 5 Incremental Software Builds, 2 Major Releases, 3 final sub-releases
      • 5.1: Defects found by I&T and 3DOF
      • 5.2: Defects found by Mission Operations Testing
      • 5.3: Final RTS set for Golden Load
  • Leverage Heritage Software

    • GOTS: GSFC OSAL, cFE, cFS, ITOS
    • MOTS: Broad Reach Drivers
    • COTS: , VxWorks, Mathworks Matlab/Simulink & associated toolboxes


Develop Models of FSW, Vehicle, and Environment

  • Develop Models of FSW, Vehicle, and Environment

  • Automatically generate High-Level Control Software

  • Integrate with hand-written and heritage software.

  • Iterate while increasing fidelity of tests – Workstation Sim (WSIM), Processor-In-The-Loop (PIL), Hardware-in-the-Loop (HIL)

  • Automated self-documenting tests providing traceability to requirements





Model-Based Development with significant software re-use: - Hype or Help?

  • Model-Based Development with significant software re-use: - Hype or Help?

  • Advantages:

  • High level control software in the “Native Language” for GN&C developers

  • Allowed development to be highly parallelized

    • Modular design for all applications, Simulink or hand-developed
    • Software developers could prototype autocode/integration process independent of Simulink module development
    • Early Requirements definition led to ability to formalize test infrastructure early in development cycle.
  • Easy to communicate design/algorithms/data flow with stakeholders and other subsystems.

  • Simulink Report generator is an extremely powerful tool for driving verification system.

  • Generated code was generally clean and efficient.



Disadvantages:

  • Disadvantages:

  • Have to be very careful when patching Simulink applications. Must upload associated parameter table. Cannot change interfaces/buses in flight.

  • Bus changes during development induced significant rework of test harnesses.

  • Personal Experience from a Simulink Newbee: LADEE Propulsion Model

  • Surprisingly fast to model. Amenable to modular development.

  • Think carefully about flow and propagation of signals. Painful to update models/test harnesses.

  • Absolutely needed advice/example models from Simulink expert because of the complexity, range of modeling choices/parameters and their effects on the autocode.

  • Lesson: Model-Based Development is effective when used in a highly disciplined manner. Sloppy development practices lead to bad outcomes, no matter what the language.



My Perspective:

  • My Perspective:

  • Daunting set of rules/regulations/practices that have arisen from lessons learned and bad outcomes from other projects.

  • They are an effective roadmap/checklist that help guide on how to plan and document our solutions to prevent those problems.

  • Strategy: Comply as simply and effectively as possible.

  • Lesson Learned:

  • Safety and Mission Assurance/Independent Reviewers can be a real ally

    • Providing templates and advice about effective practices.
    • Extra experienced eyes during the planning phase leads to fewer process issues and software defects later.
    • Early understanding by SMA/IR of project practices leads to smoother and more effective reviews.
  • When you get to the inevitable time crunch at a critical milestone, it is essential to have practiced, documented processes.

    • Multiple examples in LADEE of schedule being brought in by well-practiced test program


Our “final” 2 build cycles (4 & 5) were major deliveries to the spacecraft.

  • Our “final” 2 build cycles (4 & 5) were major deliveries to the spacecraft.

  • We smugly delivered them “Just In Time” to meet I&T schedule needs.

  • MOS “Just In Time” schedule not tied to these releases.

  • From a FSW perspective, this delayed discovery of:

    • More defects in EDICD/Fault management logic.
    • Hidden Requirements on the spacecraft simulator model.
    • Our concept of “Test Like You Fly” was not the way MOS actually flew.
  • More importantly, the schedule was not tied to “Golden Load” deadline

    • Milestones for development and certification of MOS RTSs were scheduled for after the need date for inclusion in the “golden load”.
    • Schedule Catch 22: They needed the “golden load” to certify the RTSs for inclusion in the golden load.
    • This put FSW back on the critical path for the spacecraft launch date!
  • Lessons Learned:

  • “Just in Time” philosophy leaves no room for missed schedule dependencies

  • We missed valuable test time of the end-to-end operation of the spacecraft leading to a delay in identifying defects. Some were simply too late too be incorporated in the “golden load”









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