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  • 1
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    Self-stabilized theodolite for manual tracking using photosensitive stabilizing means Patent (1966)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Self-stabilized vernier theodolite for determining angular orientation of line of sight between target and inertial reference system on manned space vehicle
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    Future timing accuracy requirements and procedures for data processing (1978)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Timing accuracy requirements for satellite experiment data are discussed. Although time accuracies of 100 milliseconds were sufficient when OSO-3, 4, 5 were launched in the mid-60s, time accuracies of 100 microseconds are necessary for OSO-8, HEAO-A, and Seasat, and it is thought likely that accuracies of 10 microseconds will become routine in the 1980s. An approach to the problem of identifying the sources of spacecraft timing errors - from the onboard counters to the final tagging of data - is considered.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: Data Management Symposium; Oct 18, 1977 - Oct 19, 1977; Huntsville, AL
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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