• DocumentCode
    817053
  • Title

    Control, navigation, and guidance

  • Author

    Draper, Charles Stark

  • Author_Institution
    The Charles Stark Draper Laboratory, Inc., Cambridge, MA, USA
  • Volume
    1
  • Issue
    4
  • fYear
    1981
  • fDate
    12/1/1981 12:00:00 AM
  • Firstpage
    4
  • Lastpage
    17
  • Abstract
    Self-contained systems providing control and navigation for vehicles of all kinds use gyroscopic elements to maintain reference directions with respect to inertial space. Sensors for resultant gravity field and inertial reaction forces along input axes determine the vertical and also linear velocities with respect to inertial space. These components divided by an equivalent Earth radius transfer the motion to Earth coordinates in which integration gives location. Corrections for Earth´s rotation projected in and perpendicular to the horizontal plane are made as computed cosine and sine projections of Earth´s angular velocity. Current systems result with the order of fractional miles per hour performance.
  • Keywords
    Aircraft control; Inertial navigation; Gyroscopes; Navigation; Sensors; Velocity control;
  • fLanguage
    English
  • Journal_Title
    Control Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0272-1708
  • Type

    jour

  • DOI
    10.1109/MCS.1981.1100795
  • Filename
    1100795