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Kinematic functions for redundancy resolution using configuration controlThe invention fulfills new goals for redundancy resolution based on manipulator dynamics and end-effector characteristics. These goals are accomplished by employing the recently developed configuration control approach. Redundancy resolution is achieved by controlling the joint inertia matrix of the end-effector mass matrix that affect the inertial torques or by reducing the joint torques due to gravity loading and payload. The manipulator mechanical-advantage and velocity-ratio are also used as performance measures to be improved by proper utilization of redundancy. Furthermore, end-effector compliance, sensitivity, and impulsive force at impact are introduced as redundancy resolution criteria. The new goals for redundancy resolution allow a more efficient utilization of the redundant joints based on the desired task requirements.
Document ID
19940025001
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Seraji, Homayoun
(NASA Pasadena Office CA, United States)
Date Acquired
August 16, 2013
Publication Date
March 15, 1994
Subject Category
Cybernetics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-967083
Patent Number: NASA-CASE-NPO-18608-1-CU
Patent Number: US-PATENT-5,294,873
Accession Number
94N29504
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-NPO-18608-1-CU|US-PATENT-5,294,873
Patent Application
US-PATENT-APPL-SN-967083
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