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  • 1
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-27
    Description: The results of an analytical investigation of the rotational dynamics of a spinning Skylab space station are presented. The passive stability of motion of a simplified model consisting of a rigid core body with two attached flexible appendages is investigated. The parameter plane stability technique is applied to the specific Skylab case to determine its transient response to external disturbances.
    Keywords: NAVIGATION
    Type: NASA-TM-X-64646
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-27
    Description: The results are presented of a study of the dynamics of a spinning Skylab space station. The stability of motion of several simplified models with flexible appendages was investigated. A digital simulation model that more accurately portrays the complex Skylab vehicle is described, and simulation results are compared with analytically derived results.
    Keywords: NAVIGATION
    Type: NASA-TM-X-64635
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-27
    Description: Development and characteristics of attitude and pointing control system for Skylab space station
    Keywords: NAVIGATION
    Type: NASA-TN-D-6068 , M-211
    Format: application/pdf
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  • 4
    Publication Date: 2019-07-13
    Description: A new approach to digital control system design is applied to the analysis and design of a practical onboard digital attitude control system for a class of spinning vehicles characterized by a rigid body and two connected flexible appendages. The approach used is to design a continuous-data control system that will provide a satisfactory system response. Then, using the digital redesign method, a digital controller with onboard digital computer is designed to provide a digital control system whose states are similar to those of the continuous system at sampling instants. The simplicity of application of this approach is indicated by an example in which spinning Skylab parameters are used to substantiate the conclusions.
    Keywords: NAVIGATION
    Type: AIAA PAPER 73-894 , Guidance and Control Conference; Aug 20, 1973 - Aug 22, 1973; Key Biscayne, FL
    Format: text
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  • 5
    Publication Date: 2019-07-13
    Description: Pointing control system /PCS/ for Apollo Telescope Mount /ATM/ for solar observations
    Keywords: NAVIGATION
    Type: AIAA PAPER 67-534 , GUIDANCE, CONTROL AND FLIGHT DYNAMICS CONFERENCE; Aug 14, 1967 - Aug 16, 1967; HUNTSVILLE, AL|; UGREVUE(
    Format: text
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  • 6
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    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Skylab earth-orbiting manned space station attitude and pointing control systems design
    Keywords: NAVIGATION
    Type: WESTERN SPACE CONGRESS ON SPACE SCIENCES - FUTURE APPLICATIONS FOR MANKIND; Oct 27, 1970 - Oct 29, 1970; SANTA MARIA, CA
    Format: text
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