NASA NTRS · 19910017213
Constrained trajectory optimization for kinematically redundant arms
Abstract
Two velocity optimization schemes for resolving redundant joint configurations are compared. The Extended Moore-Penrose Technique minimizes the joint velocities and avoids obstacles indirectly by adjoining a cost gradient to the solution. A new method can incorporate inequality constraints directly to avoid obstacles and singularities in the workspace. A four-link arm example is used to illustrate singularity avoidance while tracking desired end-effector paths.
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Carignan, Craig R., Tarrant, Janice M.. 1990-01-01. Constrained trajectory optimization for kinematically redundant arms. https://ntrs.nasa.gov/citations/19910017213
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