weighted factor method中文是什么意思

發(fā)音:

中文翻譯
造句

加權(quán)因數(shù)法
加權(quán)因子法

weight n. 1.重量；體重；求心力，重力，(地心)引力。 2. ...
factor n. 1.〔英國(guó)〕經(jīng)銷(xiāo)人；(代客買(mǎi)賣(mài)收取傭金的)經(jīng)紀(jì)人； ...
method n. 1.方法，方式；順序。 2.(思想、言談上的)條理 ...
weighted factor 加權(quán)系數(shù); 加權(quán)因素; 加權(quán)因子
weighted method 加權(quán)法
effective weighted factor 有效加權(quán)系數(shù)
weighted distortion factor 加權(quán)失真因數(shù)
weighted flow factor 加權(quán)水流因數(shù)
method of weighted least squares 加權(quán)最小二乘法
method of weighted mean 加權(quán)平均法
method of weighted residual 加權(quán)殘差法; 加權(quán)殘數(shù)法
method of weighted residuals 加權(quán)余量法
moving weighted average method 移動(dòng)加權(quán)平均法
the weighted-average method 加權(quán)平均法
weighted average inventory method 加權(quán)平均存貨法
weighted average method 加權(quán)平均法
weighted averages method 加權(quán)平均法（指存貨的計(jì)價(jià)）
weighted centroid simplex method 加權(quán)質(zhì)心單形法; 加權(quán)質(zhì)心簡(jiǎn)捷法
weighted in points method 加權(quán)計(jì)分法
weighted least square method 加權(quán)最小平方法; 加權(quán)最玄乘法
weighted least squares method 加權(quán)最小二乘法
weighted least-squares method 加權(quán)最小二乘法
weighted linear regression method 加權(quán)直線回歸法
weighted market capitalization method 加權(quán)資本市值法
weighted mean method 加權(quán)平均法

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Based on optimal control theory and singularly perturbed theory , a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed . this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method , minimum energy cruising phase control and minimum energy switching phase control . moreover , a new control logic is designed in order to remove influence of climbing control on switching phase . simulation results of a certain type of air - to - ground missile are presents . it is shown that , with simple control algorithm and feasible onboard implementation , this law not only guarantees air - to - ground missiles to ascent quickly , but also satisfies the requirements of midcourse phases . the studies have important theoretical meaning and great value of engineering application
為滿足實(shí)際作戰(zhàn)的要求，基于最優(yōu)控制理論和奇異攝動(dòng)方法，提出了一種可保證中遠(yuǎn)程空地導(dǎo)彈快速爬升到最優(yōu)高度的中制導(dǎo)律.它由變系數(shù)最優(yōu)爬升控制，最小能量巡航控制和最小能量下滑控制組成.為了減小爬升段控制對(duì)下滑段的影響，提出了一種新的控制邏輯.最后針對(duì)某型空地導(dǎo)彈進(jìn)行了仿真.結(jié)果表明，該中制導(dǎo)律較好地滿足了中遠(yuǎn)程空地導(dǎo)彈在中制導(dǎo)段的要求.本文的研究結(jié)果具有較好地工程參考價(jià)值
Abstract : based on optimal control theory and singularly perturbed theory , a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed . this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method , minimum energy cruising phase control and minimum energy switching phase control . moreover , a new control logic is designed in order to remove influence of climbing control on switching phase . simulation results of a certain type of air - to - ground missile are presents . it is shown that , with simple control algorithm and feasible onboard implementation , this law not only guarantees air - to - ground missiles to ascent quickly , but also satisfies the requirements of midcourse phases . the studies have important theoretical meaning and great value of engineering application
文摘:為滿足實(shí)際作戰(zhàn)的要求，基于最優(yōu)控制理論和奇異攝動(dòng)方法，提出了一種可保證中遠(yuǎn)程空地導(dǎo)彈快速爬升到最優(yōu)高度的中制導(dǎo)律.它由變系數(shù)最優(yōu)爬升控制，最小能量巡航控制和最小能量下滑控制組成.為了減小爬升段控制對(duì)下滑段的影響，提出了一種新的控制邏輯.最后針對(duì)某型空地導(dǎo)彈進(jìn)行了仿真.結(jié)果表明，該中制導(dǎo)律較好地滿足了中遠(yuǎn)程空地導(dǎo)彈在中制導(dǎo)段的要求.本文的研究結(jié)果具有較好地工程參考價(jià)值

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