contained parameter 中文意思是什麼

contained parameter 解釋
內含參數
  • contained : 包含的
  • parameter : n. 1. 【數學】參數,變數;參詞;參項。2. 【物理學】參量;(結晶體的)標軸。3. 〈廢語〉【天文學】通徑。vt. -ize 使參數化。
  1. The ability for the server to deserialize the encoded parameter contained within the envelope

    服務器對信封中包含的已編碼參數進行無序化處理的能力。
  2. A parameter known as the " mass density " - that is, how much matter per unit volume is contained in the universe - determines which of the three possibilities applies to the universe

    以「質量密度」聞名的一個參數-也就是,在宇宙里含有多少單位體積物質?確定三種可能性哪一種適用於宇宙。
  3. When you pass a delegate as a parameter, or pass a delegate contained as a field in a structure, it remains uncollected for the duration of the call

    如果委託作為參數進行傳遞,或者所包含的委託作為結構中的欄位進行傳遞,則該委託在調用期間不會被回收。
  4. Parameter is contained within the visible clip region of this

    的可見剪輯區域內,則為
  5. The paper involved follow contents : a. introduced the basic theory of some basis theories about the layout to materials handling systems ; b. developed a cad software, in the development, the follow technical problem : 1 ) found the self - contained graphic and parameter aggregate of the equipment according to the work system of ksec ; 2 ) realized the parametric designing and changing of the mhs equipment by developing autocad using the vba as the tool ; c

    論文主要包括以下內容: 1 、對物流系統規劃的有關理論作了介紹; 2 、開發了計算機輔助設計軟體,在軟體開發中主要解決了以下技術問題: a )根據昆船物流公司的工程標準建立了完備的設備圖形庫及設備參數數據庫, b )通過vba對autocad進行二次開發,實現了各種設備的參數化設計並可以完成自動修改。
  6. First, being based upon kalman filter, extended kalman filter formulas was established ; second, with using extended kalman filter in non - linear dynamics system maximum likelihood identification method, the self - contained formulas of estimating parameter was established ; third, according to the air layout of the missle, the aerodynamic parameters identification calculating model was gained, with applying to the non - linear dynamics system maximum likelihood identification method ; finally, with using the calculating model, the aerodynamic parameters were gained. the results which were gained from the calulating model were almost consistent with which were gained from the wind tunnel experiment. thus, it was viable to use the method to estimate the aerodynamic parameters

    首先,以卡爾曼濾波為基礎,將其推廣于非線性動力學系統,建立了廣義卡爾曼濾波算式;其次,把廣義卡爾曼濾波算式應用於非線性動力學系統最大似然演算法和非線性動力學系統最大似然遞推演算法中,建立了各自的參數估計完備算式;再其次,以所建立的傾斜穩定導彈空間運動數學模型為基礎,根據該導彈的氣動布局,推導並建立了該導彈空間運動數學模型,將最大似然遞推演算法應用其中,建立了導彈氣動力參數辨識的數學模型;最後,利用該模型,估算出了氣動力參數,所得結果與風洞實驗數據基本吻合,從而認為採用此方法是可行的。
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