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タイトルKinematic functions for redundancy resolution using configuration control
本文(外部サイト)http://hdl.handle.net/2060/19940025001
著者(英)Seraji, Homayoun
著者所属(英)Jet Propulsion Lab., California Inst. of Tech.; NASA Pasadena Office
発行日1994-03-15
言語eng
内容記述The 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.
NASA分類CYBERNETICS
レポートNO94N29504
権利No Copyright


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