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  • 1
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    The near field of the instrument landing system glide slope. (1968)
    In:  Other Sources
    Details
    Publication Date: 2011-08-12
    Description: Aircraft instrument landing system glide slope pattern near airport runway, noting glide slope antenna directivity effect
    Keywords: NAVIGATION
    Type: ; ADEMIE DES SCIENCES
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    Self-Test Techniques for Redundant Data Management Systems (1971)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: Characteristics of Space shuttle data management system for data transmission and service for avionics equipment and other subsystems
    Keywords: COMPUTERS
    Type: NASA. Manned Spacecraft Center Proc. of the Space Shuttle Integrated Electron. Conf., Vol. 3; p 309-328
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Apollo lunar ascent and descent. (1967)
    In:  Other Sources
    Details
    Publication Date: 2018-12-01
    Description: Lunar module onboard guidance equipment design, noting operational strategies, control systems, etc
    Keywords: NAVIGATION
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Space processing applications payload equipment study. Volume 2C: Data acquisition and process control (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The services provided by the Spacelab Information Management System are discussed. The majority of the services are provided by the common-support subsystems in the Support Module furnished by the Spacelab manufacturer. The information processing requirements for the space processing applications (SPA) are identified. The requirements and capabilities for electric power, display and control panels, recording and telemetry, intercom, and closed circuit television are analyzed.
    Keywords: SPACE VEHICLES
    Type: NASA-CR-120344 , TRW-22886-6034-RU-02-VOL-2C
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    Design of a GN and C system to meet reliability goals (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: This paper analyzes the reliability of the guidance, navigation, and control (GNC) portion of an avionics system for the Space Shuttle Orbiter. This analysis shows how the GNC design is affected by the need to achieve an acceptable probability of successful completion of a mission and of safe return to an airport. It varies the redundancy of the inertial measurement unit (IMU), computers, and other time-critical elements. It also includes the reliability of the flight control electronics and of the nontime-critical sensors on a phase-by-phase basis. It shows that quadruple redundancy in certain subsystems, high quality parts, and cross-strapping on orbit are required.
    Keywords: NAVIGATION
    Type: Annual Reliability and Maintainability Symposium; Jan 29, 1974 - Jan 31, 1974; Los Angeles, CA
    Format: text
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    NASA TECHNICAL REPORTS
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