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
Link To Document :
بازگشت