• DocumentCode
    1462582
  • Title

    Inertial systems in space vehicles

  • Author

    Matthews, M.A.V.

  • Volume
    22
  • Issue
    3
  • fYear
    1961
  • fDate
    9/1/1961 12:00:00 AM
  • Firstpage
    231
  • Lastpage
    239
  • Abstract
    This paper discusses the use of inertial elements in space vehicles for attitude control and navigation. Some limitations of inertial systems in this environment are described and it is shown that inertia alone is not adequate for most space applications. However, the use of inertia to bridge the gaps between information from other sources can simplify the requirements for other sensors in the satellite, and also on the ground tracking equipment. This is illustrated by some examples and by discussion of space vehicle.
  • Keywords
    artificial satellites;
  • fLanguage
    English
  • Journal_Title
    Radio Engineers, Journal of the British Institution of
  • Publisher
    iet
  • Type

    jour

  • DOI
    10.1049/jbire.1961.0111
  • Filename
    5259653