two-level allocation in Chinese
Translation
Mobile
- 二級(jí)分配
- "two" in Chinese : n. (pl. twos) 1.兩人;兩個(gè)東西,一對。 ...
- "level" in Chinese : n. 1.水平儀,水準(zhǔn)儀;水準(zhǔn)測量。 2.水平線,水平面 ...
- "allocation" in Chinese : n. 1.(原料等的)分配,配給。 2.配給物,配給量。 ...
- "flight level allocation" in Chinese : 飛行高度層的分配
- "two-level" in Chinese : 雙層的; 雙域值
- "addressing two-level" in Chinese : 二階尋址
- "law of two level game" in Chinese : 雙層游戲規(guī)則
- "lcache ,level two cache" in Chinese : 二級(jí)緩存
- "simple two-level" in Chinese : 采樣如果場景中只有少量部分需要抗鋸齒
- "the level of the two is quite different" in Chinese : 兩個(gè)人的水平相差很遠(yuǎn)
- "two level action" in Chinese : 雙位置動(dòng)作
- "two level address" in Chinese : 二階位址
- "two level addressing" in Chinese : 二級(jí)定址; 二級(jí)尋址
- "two level autocorrelation function" in Chinese : 雙值自相關(guān)函數(shù)
- "two level code" in Chinese : 二電平碼
Examples
- Abstract : a new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
文摘:探討了一種新的設(shè)計(jì)指標(biāo)最優(yōu)分配方法- -協(xié)同分配法,用于處理飛機(jī)頂層設(shè)計(jì)中的大規(guī)模設(shè)計(jì)指標(biāo)最優(yōu)分配問題.分析了飛機(jī)頂層設(shè)計(jì)中的設(shè)計(jì)指標(biāo)最優(yōu)分配特征,據(jù)此給出了協(xié)同法的原理并建立了數(shù)學(xué)模型.協(xié)同法按設(shè)計(jì)指標(biāo)分配關(guān)系將最優(yōu)分配問題分解為主系統(tǒng)優(yōu)化和子系統(tǒng)優(yōu)化,主優(yōu)化對子系統(tǒng)設(shè)計(jì)指標(biāo)進(jìn)行最優(yōu)分配,子優(yōu)化以最小化分配設(shè)計(jì)指標(biāo)值與期望設(shè)計(jì)指標(biāo)值之間的差異為目標(biāo),進(jìn)行子系統(tǒng)最優(yōu)設(shè)計(jì),或?qū)Φ讓釉?如飛機(jī)翼梁、翼肋和翼盒等)進(jìn)行設(shè)計(jì)指標(biāo)最優(yōu)分配,并把最優(yōu)解信息反饋給主優(yōu)化.主優(yōu)化通過子優(yōu)化最優(yōu)解信息構(gòu)成的一致性約束協(xié)調(diào)分配量,提高系統(tǒng)整體性能,并重新給出分配方案.主系統(tǒng)與子系統(tǒng)反復(fù)協(xié)調(diào),直到得到設(shè)計(jì)指標(biāo)最優(yōu)分配方案.兩層可靠度指標(biāo)分配算例初步驗(yàn)證了本文方法的正確性與可行性,三層可靠度指標(biāo)分配算例證明了本文方法的有效性.最后,以重量指標(biāo)分配為例,簡要敘述了針對飛機(jī)頂層設(shè)計(jì)中設(shè)計(jì)指標(biāo)協(xié)同分配的數(shù)學(xué)模型和求解思路 - A new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
探討了一種新的設(shè)計(jì)指標(biāo)最優(yōu)分配方法- -協(xié)同分配法,用于處理飛機(jī)頂層設(shè)計(jì)中的大規(guī)模設(shè)計(jì)指標(biāo)最優(yōu)分配問題.分析了飛機(jī)頂層設(shè)計(jì)中的設(shè)計(jì)指標(biāo)最優(yōu)分配特征,據(jù)此給出了協(xié)同法的原理并建立了數(shù)學(xué)模型.協(xié)同法按設(shè)計(jì)指標(biāo)分配關(guān)系將最優(yōu)分配問題分解為主系統(tǒng)優(yōu)化和子系統(tǒng)優(yōu)化,主優(yōu)化對子系統(tǒng)設(shè)計(jì)指標(biāo)進(jìn)行最優(yōu)分配,子優(yōu)化以最小化分配設(shè)計(jì)指標(biāo)值與期望設(shè)計(jì)指標(biāo)值之間的差異為目標(biāo),進(jìn)行子系統(tǒng)最優(yōu)設(shè)計(jì),或?qū)Φ讓釉?如飛機(jī)翼梁、翼肋和翼盒等)進(jìn)行設(shè)計(jì)指標(biāo)最優(yōu)分配,并把最優(yōu)解信息反饋給主優(yōu)化.主優(yōu)化通過子優(yōu)化最優(yōu)解信息構(gòu)成的一致性約束協(xié)調(diào)分配量,提高系統(tǒng)整體性能,并重新給出分配方案.主系統(tǒng)與子系統(tǒng)反復(fù)協(xié)調(diào),直到得到設(shè)計(jì)指標(biāo)最優(yōu)分配方案.兩層可靠度指標(biāo)分配算例初步驗(yàn)證了本文方法的正確性與可行性,三層可靠度指標(biāo)分配算例證明了本文方法的有效性.最后,以重量指標(biāo)分配為例,簡要敘述了針對飛機(jī)頂層設(shè)計(jì)中設(shè)計(jì)指標(biāo)協(xié)同分配的數(shù)學(xué)模型和求解思路
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