发明名称 PARAMETER CORRECTION METHOD AND CONTROL SYSTEM
摘要 PROBLEM TO BE SOLVED: To make a control object whose position attitude is determined by x, y, z, α, &bgr;, γ a position attitude of a target.SOLUTION: N actual position attitudes V(n) and a position attitude V(T) of a target are defined as n reference points P(n) and a first correction target point P(T) of a sixth-dimensional coordinate system. Seven first reference points P(n) constituting a sixth-dimensional simple substance including the first correction target point P(T) are specified. The seven first reference points P(n) and the first correction target point P(T) are converted into seven second reference points P'(n) and a second correction target point P'(T) of a seventh-dimensional coordinate system obtained by adding an error component &Dgr;x axis to the sixth-dimensional coordinate system. A hyperplane R(&Dgr;x) including the seven second reference points P'(n) is calculated, and the second correction target point P'(T) is substituted into the hyperplane R(&Dgr;x) to calculate an error component &Dgr;x(T). Similarly, &Dgr;y(T), &Dgr;z(T), &Dgr;α(T), &Dgr;&bgr;(T), &Dgr;γ(T) are calculated, and parameters are corrected so as to be a position attitude of the target on the basis of the error components.
申请公布号 JP2013131149(A) 申请公布日期 2013.07.04
申请号 JP20110281865 申请日期 2011.12.22
申请人 KAWASAKI HEAVY IND LTD 发明人 NAKAMURA NAOHIRO;HONDA FUMIHIRO;KUBOTA TETSUYA
分类号 G05B19/404;B25J9/10 主分类号 G05B19/404
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