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Multirate and event-driven Kalman filters for helicopter flightA 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.
Document ID
19930071763
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Sridhar, Banavar
(NASA Ames Research Center Moffett Field, CA, United States)
Smith, Phillip
(NASA Ames Research Center Moffett Field, CA, United States)
Suorsa, Raymond E.
(NASA Ames Research Center Moffett Field, CA, United States)
Hussien, Bassam
(Sterling Federal Systems Group Palo Alto, CA, United States)
Date Acquired
August 16, 2013
Publication Date
August 1, 1993
Publication Information
Publication: IEEE Control Systems Magazine
Volume: 13
Issue: 4
ISSN: 0272-1708
Subject Category
Aircraft Instrumentation
Accession Number
93A55760
Distribution Limits
Public
Copyright
Other

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