- 加權(quán)因數(shù)法
- 加權(quán)因子法
下載手機詞典可隨時隨地查詞查翻譯
weighted factor method中文什么意思
例句與用法
- 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(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(dǎo)彈進行了仿真.結(jié)果表明，該中制導(dǎo)律較好地滿足了中遠程空地導(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(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(dǎo)彈進行了仿真.結(jié)果表明，該中制導(dǎo)律較好地滿足了中遠程空地導(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值