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weighted factor method中文是什么意思
- 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〕經(jīng)銷人；(代客買賣收取傭金的)經(jīng)紀人； ...
- 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（指存貨的計價）
- weighted centroid simplex method 加權(quán)質(zhì)心單形法; 加權(quán)質(zhì)心簡捷法
- weighted in points method 加權(quán)計分法
- 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
- 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
為滿足實際作戰(zhàn)的要求，基于最優(yōu)控制理論和奇異攝動方法，提出了一種可保證中遠程空地導彈快速爬升到最優(yōu)高度的中制導律.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下滑段的影響，提出了一種新的控制邏輯.最后針對某型空地導彈進行了仿真.結(jié)果表明，該中制導律較好地滿足了中遠程空地導彈在中制導段的要求.本文的研究結(jié)果具有較好地工程參考價值 - 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:為滿足實際作戰(zhàn)的要求，基于最優(yōu)控制理論和奇異攝動方法，提出了一種可保證中遠程空地導彈快速爬升到最優(yōu)高度的中制導律.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下滑段的影響，提出了一種新的控制邏輯.最后針對某型空地導彈進行了仿真.結(jié)果表明，該中制導律較好地滿足了中遠程空地導彈在中制導段的要求.本文的研究結(jié)果具有較好地工程參考價值
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