• DocumentCode
    332534
  • Title

    Implementation and testing of International Space Station flight software for the pointing and support portion of guidance, navigation and control

  • Author

    Yazell, Douglas J.

  • Author_Institution
    Commercial Syst. Oper., Honeywell Space Syst., Houston, TX, USA
  • Volume
    1
  • fYear
    1998
  • fDate
    31 Oct-7 Nov 1998
  • Abstract
    Boeing engineers designed and implemented these algorithms using MOODS (Multibody On-Orbit Dynamics Simulation), a Boeing/NASA Ada non-realtime simulation running on a DEC Alpha platform in Boeing Tower 2 in Houston, Texas. The Ada flight software was then written in MatrixX superblocks on Hewlett Packard computers, using the MatrixX autocode capability to generate the Ada code. After Flight Stage 5A of the International Space Station (ISS), the Pointing and Support (P&S) subsystem is activated and provides the Guidance, Navigation, and Control (GN&C) interface for most of the other U.S. subsystems. P&S supplies state vector (ISS position and velocity), attitude, and attitude rate data to other ISS systems
  • Keywords
    aerospace simulation; aerospace testing; attitude control; program testing; space vehicles; Ada nonrealtime simulation; DEC Alpha platform; International Space Station flight software; MOODS; MatrixX autocode capability; MatrixX superblocks; attitude rate data; guidance; multibody on-orbit dynamics simulation; navigation; pointing; space vehicle control; state vector; support portion; Aerospace engineering; Algorithm design and analysis; Automatic programming; Computational modeling; Design engineering; International Space Station; Mood; NASA; Poles and towers; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
  • Conference_Location
    Bellevue, WA
  • Print_ISBN
    0-7803-5086-3
  • Type

    conf

  • DOI
    10.1109/DASC.1998.741486
  • Filename
    741486