Research Catalog

  • Uncertainty analysis of inertial model attitude sensor calibration and application with a recommended new calibration method [microform] / John S. Tripp and Ping Tcheng.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Dynamic response tests of inertial and optical wind-tunnel model attitude measurement devices [microform] / R.D. Buehrle.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • High-precision buffer circuit for suppression of regenerative oscillation [microform] / John S. Tripp, David A. Hare, and Ping Tcheng.

    • Text
    • [Hampston, Va.] : NASA, Langley Research Center ; [Springfield, VA : National Technical Information Service, distributor, 1995]
    • 1995
  • A control design for the attitude control and determination system for the Magnetosphere Imager spacecraft [microform] / M.E. Polites and C.K. Carrington.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Attitude Determination Error Analysis System (ADEAS) mathematical specification document [microform] / prepared by Computer Sciences Corporation ; M. NIcholson, F. Markley, E. Seidewitz.

    • Text
    • [Greenbelt, Md.] : Goddard Space Flight Center, [1988?]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69659
  • Infrared horizon sensor modeling for attitude determination and control [microform] : analysis and mission experience / M.C. Phenneger ... [et al.].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96599
  • A study on airborne integrated display system and human information processing [microform] / K. Mizumoto ... [et al.].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983
  • Design, development, and test-flight of the Rayleigh Scattering Attitude Sensor / E. Hilsenrath [and eight others].

    • Text
    • Greenbelt, Maryland : National Aeronautics and Space Administration, Goddard Space Flight Center, September 1997.
    • 1997-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66739

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