Last edited by Maubei
Friday, April 24, 2020 | History

3 edition of Optimal control theory determination of feasible return-to-launch-site aborts for the HL-20 personnel launch system vehicle found in the catalog.

Optimal control theory determination of feasible return-to-launch-site aborts for the HL-20 personnel launch system vehicle

Optimal control theory determination of feasible return-to-launch-site aborts for the HL-20 personnel launch system vehicle

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

    Subjects:
  • Space vehicles -- Attitude control systems.

  • Edition Notes

    StatementKevin E. Dutton.
    SeriesNASA technical paper -- 3449.
    ContributionsLangley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17682186M


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