robustness analysis造句
例句與造句
- robustness analysis of the ifn-induced jak-stat signaling pathway
干擾素誘導(dǎo)的jak-stat信號通路的魯棒性分析 - design of a class of self-learning fuzzy controller and its robustness analysis
一類自學(xué)習(xí)模糊控制器的設(shè)計(jì)及魯棒性分析 - the guaranteed cost control and the robustness analysis for the uncertain time delay systems
時滯不確定系統(tǒng)保成本控制及魯棒性分析 - robustness analysis of responses of vibration control structures with uncertain parameters
不確定參數(shù)結(jié)構(gòu)振動控制系統(tǒng)響應(yīng)的魯棒性分析 - robustness analysis and output feedback control for strictly positive real linear mimo systems
嚴(yán)格正實(shí)線性多變量系統(tǒng)的魯棒性分析及其輸出反饋控制 - It's difficult to find robustness analysis in a sentence. 用robustness analysis造句挺難的
- here, the issue of robustness analysis of cell jak-stat signal transduction networks is addressed
因此我們有必要研究細(xì)胞在不同生理狀況下的變化情況。 - robustness analysis of the stability of the second order control systems with uncertainties using interval method
基于區(qū)間方法的不確定二階控制系統(tǒng)穩(wěn)定性的魯棒性分析 - controller tuning and testing including stability and robustness analysis . 4 . test results to the implementation of mpc for spacecraft control
對控制器的調(diào)試和測試(包括對控制器的穩(wěn)定性和魯棒性的分析)。 - this is investigated upon a mathematical model of ifn-induced jak-stat signaling pathway by applying robustness analysis which is based on a broad range of simultaneous and systematical parameters variation
我們對細(xì)胞的jak-stat信號建立了數(shù)學(xué)模型，同時系統(tǒng)地改變模型中的動力學(xué)參數(shù)反應(yīng)速率參數(shù)，然后進(jìn)行大量的數(shù)值模擬實(shí)驗(yàn)。 - the current control approaches are based on frequency domain methods such as pid control which assumes linear time invariant system dynamics . the advantages of these approaches are simplicity and ease of stability and robustness analysis . however, the decrease in performanc e and poor efficiency translates to additional payload and cannot meet the demand of current spacecraft control
當(dāng)前飛行器主要的控制方法是基于近似時不變線性系統(tǒng)的頻域分析法(如pid控制)，這種方法的優(yōu)點(diǎn)是簡單且易于穩(wěn)定性和魯棒性分析，但它所達(dá)到的低性能和低效率卻轉(zhuǎn)化成了飛行器控制過程的附加載荷，還遠(yuǎn)不夠滿足當(dāng)前飛行器控制的要求。