Continuous path control of space manipulators mounted on OMV

Yoji Umetani, Kazuya Yoshida

研究成果: Article査読

112 被引用数 (Scopus)

抄録

Theoretical analysis on the formulation of kinematics for the manipulator mounted on a satellite is presented. Firstly, to solve the inverse kinematics, the authors define a new generalized Jacobian matrix, and utilizing this generalized matrix, the problem can be treated analytically. Secondly, the authors verify the method proposed here in the simulation study. Thirdly, they also discuss on the several points which are indispensable for further investigations.

本文言語English
ページ(範囲)981-986
ページ数6
ジャーナルActa Astronautica
15
12
DOI
出版ステータスPublished - 1987 12
外部発表はい

ASJC Scopus subject areas

  • Aerospace Engineering

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