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  • 1
    Publication Date: 2019-06-27
    Description: The underlying theory and design of test instrumentation and computer techniques used to determine the power spectral density (PSD) of the third generation gyro are described in detail. Acceptance test results on the completed instrument are presented as well as composite PSD plots. The measured RMS noise over the frequency band 0.0025 - 10 Hz was 0.012 arc seconds. Results obtained at Martin Company indicate an RMS noise of 0.009 arc seconds (0.05 - 10 Hz). The results obtained showed the TGG performance was close to the proposed LST requirements but that additional development work would be needed to reduce the TGG noise to within more desirable limits.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-CR-143973 , R-896
    Format: application/pdf
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  • 2
    Publication Date: 2019-08-14
    Description: No abstract available
    Keywords: Instrumentation and Photography
    Type: NASA-CR-158637 , R-746-VOL-4
    Format: application/pdf
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  • 3
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    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Optimal axis alignment for strapdown inertial guidance system, suggesting alternate method of raised mounting pads and cylindrical alignment pins
    Keywords: NAVIGATION
    Type: PROBLEMS IN INERTIAL GUIDANCE MEETING; Jan 21, 1970 - Jan 22, 1970; CAMBRIDGE, MA
    Format: text
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