DocumentCode
2491755
Title
Planetary terminal descent hazard avoidance using optical flow
Author
Hoff, William ; Sklair, Cheryl
Author_Institution
Martin Marietta Astronaut. Group, Denver, CO, USA
fYear
1990
fDate
13-18 May 1990
Firstpage
238
Abstract
An algorithm that uses optical flow to detect landing hazards for a descending spacecraft is described. Image edge points are tracked between frames of a motion sequence, and the range to the points is calculated from the displacement of the edge points and the known motion of the camera. A novel variable-sized edge detector is used to compensate for the change in distance from one image to the next. Kalman filtering is used to incrementally improve the range estimates to those points and provide an estimate of the uncertainty in each range. Errors in camera motion and image point measurement are also modeled. A surface is then interpolated to these points, providing a complete map from which hazards such as steeply sloping areas can be detected. The algorithm has been applied to synthetic and real image sequences, with resulting range accuracy on the order of 1-3% of the range
Keywords
Kalman filters; aerospace computing; computerised pattern recognition; computerised picture processing; space vehicles; Kalman filtering; camera; complete map; descending spacecraft; edge points; hazards; landing hazards; motion sequence; optical flow; range estimates; steeply sloping areas; terminal descent hazard avoidance; uncertainty; variable-sized edge detector; Cameras; Filtering; Hazards; Image edge detection; Image motion analysis; Kalman filters; Optical detectors; Optical filters; Space vehicles; Tracking;
fLanguage
English
Publisher
ieee
Conference_Titel
Robotics and Automation, 1990. Proceedings., 1990 IEEE International Conference on
Conference_Location
Cincinnati, OH
Print_ISBN
0-8186-9061-5
Type
conf
DOI
10.1109/ROBOT.1990.125979
Filename
125979
Link To Document