• DocumentCode
    929786
  • Title

    Multirate and event-driven Kalman filters for helicopter flight

  • Author

    Sridhar, B. ; Smith, P. ; Suorsa, R. ; Hussien, B.

  • Author_Institution
    NASA Ames Res. Center, Moffett Field, CA, USA
  • Volume
    13
  • Issue
    4
  • fYear
    1993
  • Firstpage
    26
  • Lastpage
    33
  • Abstract
    A vision-based obstacle detection system that provides information about objects as a function of azimuth and elevation is discussed. The range map is computed using a sequence of images from a passive sensor, and an extended Kalman filter is used to estimate range to obstacles. The magnitude of the optical flow that provides measurements for each Kalman filter varies significantly over the image depending on the helicopter motion and object location. In a standard Kalman filter, the measurement update takes place at fixed intervals. It may be necessary to use a different measurement update rate in different parts of the image in order to maintain the same signal to noise ratio in the optical flow calculations. A range estimation scheme that accepts the measurement only under certain conditions is presented. The estimation results from the standard Kalman filter are compared with results from a multirate Kalman filter and an event-driven Kalman filter for a sequence of helicopter flight images.<>
  • Keywords
    Kalman filters; computer vision; computerised navigation; helicopters; image sequences; event-driven Kalman filters; extended Kalman filter; image sequences; multirate Kalman filter; optical flow; range estimation; range map; vision-based obstacle detection system; Azimuth; Fluid flow measurement; Helicopters; Image motion analysis; Image sensors; Measurement standards; Motion measurement; Object detection; Optical filters; Optical sensors;
  • fLanguage
    English
  • Journal_Title
    Control Systems, IEEE
  • Publisher
    ieee
  • ISSN
    1066-033X
  • Type

    jour

  • DOI
    10.1109/37.229556
  • Filename
    229556