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Numerical Approach of Collision Avoidance and Optimal Control on Robotic ManipulatorsCollision-free optimal motion and trajectory planning for robotic manipulators are solved by a method of sequential gradient restoration algorithm. Numerical examples of a two degree-of-freedom (DOF) robotic manipulator are demonstrated to show the excellence of the optimization technique and obstacle avoidance scheme. The obstacle is put on the midway, or even further inward on purpose, of the previous no-obstacle optimal trajectory. For the minimum-time purpose, the trajectory grazes by the obstacle and the minimum-time motion successfully avoids the obstacle. The minimum-time is longer for the obstacle avoidance cases than the one without obstacle. The obstacle avoidance scheme can deal with multiple obstacles in any ellipsoid forms by using artificial potential fields as penalty functions via distance functions. The method is promising in solving collision-free optimal control problems for robotics and can be applied to any DOF robotic manipulators with any performance indices and mobile robots as well. Since this method generates optimum solution based on Pontryagin Extremum Principle, rather than based on assumptions, the results provide a benchmark against which any optimization techniques can be measured.
Document ID
19900016236
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Jyhshing Jack Wang
(The M W Kellogg Company Houston, TX, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Publication Information
Publication: Third Annual Workshop on Space Operations Automation and Robotics (SOAR 1989)
Publisher: National Aeronautics and Space Administration
Subject Category
Cybernetics
Report/Patent Number
NASA-CP-3059
Meeting Information
Meeting: 3rd Annual Workshop on Space Operations Automation and Robotics (SOAR 89)
Location: Houston, TX
Country: US
Start Date: July 25, 1989
End Date: July 27, 1989
Sponsors: National Aeronautics and Space Administration, United States Air Force
Accession Number
90N25552
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
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