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  • LAUNCH VEHICLES AND SPACE VEHICLES  (2)
  • SPACECRAFT PROPULSION AND POWER  (1)
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  • 1
    Publication Date: 2006-02-14
    Description: Future space systems, flexible spacecraft, modular control, design-test-revise cycle, and control technique verification are discussed.
    Keywords: LAUNCH VEHICLES AND SPACE VEHICLES
    Type: NASA. Langley Research Center Large Space Antenna Systems Technol., Pt. 2; p 709-719
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  • 2
    Publication Date: 2014-09-10
    Description: The MSFC facility proposed for the Space Station Attitude Control Simulator which consists of a large three degree of freedom table driven by computer controlled hydraulic actuators designed to give high bandwidth and extremely fine control through large angles is outlined. The facility includes star and solar simulators providing collimated light with the spectral content and intensity typical of Earth orbit.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: NASA. Langley Research Center Integrated Flywheel Technol., 1983; p 165-168
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  • 3
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The National Aeronautics and Space Administration (NASA) is conducting conceptual studies concerning the development of a future U.S. Space Station. The Space Station navigation, guidance, and control functions must be performed over the projected long lifetime of the station. After examining the pertinent history of U.S. spacecraft, this paper examines how these long-term operations can be achieved, settling on autonomous operations as a desirable goal. The paper concludes with a recommended development approach.
    Keywords: LAUNCH VEHICLES AND SPACE VEHICLES
    Type: AAS PAPER 83-062 , Guidance and control 1983; Feb 05, 1983 - Feb 09, 1983; Keystone, CO
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