local variables 中文意思是什麼

local variables 解釋
局部變量
  • local : adj 1 地方的,當地的,本地的。2 局部的。3 鄉土的,狹隘的,片面的。4 【郵政】本市的,本地的;【鐵...
  • variables : 變量
  1. The local variables within the current lexical scope

    當前詞法范圍內的局部變量。
  2. Initialization of local variables to a nonzero value

    將局部變量初始化為非零值。
  3. Where local variables are numbered 0 onwards

    中,其中局部變量從0向上進行編號。
  4. Unsupported changes to static local variables

    不受支持的靜態局部變量的更改
  5. Local variables are not initialized and the generated code is unverifiable

    ,則不初始化局部變量,並且生成的代碼將無法驗證。
  6. When activated, a stack probe reaches benignly into memory by the amount of space required to store the associated function s local variables

    堆棧探測激活時,它在內存中良性延伸存儲關聯函數的局部變量所需的空間量。
  7. An ole db consumer binds columns in the database tables with local variables ; to do this, it uses an

    Ole db使用者將數據庫表中的列與局部變量綁定在一起;為此,它使用
  8. Other refactoring options include encapsulating fields, promoting local variables to method parameters, and managing method parameters

    其他重構選項包括封裝欄位、將局部變量提升為方法參數以及管理方法參數。
  9. We need a uniform way to deal with generic pointers ; therefore, we prefix their names with an underscore and only use them to initialize local variables with the desired types and with the appropriate names

    我們需要一個統一的方式來處理這些通用指針,故我們用名字前面加下劃線的方法來表示這些通用指針,並且只用他們來初始化需要的特定類型和名稱的局部變量。
  10. Or any access modifiers to declare local variables

    或任何訪問修飾符來聲明局部變量。
  11. Information includes connecting to a database, creating a stored procedure, stepping into a stored procedure, setting breakpoints, viewing parameters and local variables in the locals window, and dragging variables from the text editor into the watch window

    涉及的信息包括:連接到數據庫,創建存儲過程,單步執行存儲過程,設置斷點,查看局部窗口中參數和局部變量,將變量從文本編輯器拖動到監視窗口。
  12. Empty names should be interpreted as temporary local variables during serialization

    在序列化過程中,應將空名稱解釋為臨時局部變量。
  13. A vulnerable parameter is allocated before the cookie and local variables

    易受攻擊的參數在cookie和局部變量之前分配。
  14. 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:探討了一種新的設計指標最優分配方法- -協同分配法,用於處理飛機頂層設計中的大規模設計指標最優分配問題.分析了飛機頂層設計中的設計指標最優分配特徵,據此給出了協同法的原理並建立了數學模型.協同法按設計指標分配關系將最優分配問題分解為主系統優化和子系統優化,主優化對子系統設計指標進行最優分配,子優化以最小化分配設計指標值與期望設計指標值之間的差異為目標,進行子系統最優設計,或對底層元件(如飛機翼梁、翼肋和翼盒等)進行設計指標最優分配,並把最優解信息反饋給主優化.主優化通過子優化最優解信息構成的一致性約束協調分配量,提高系統整體性能,並重新給出分配方案.主系統與子系統反復協調,直到得到設計指標最優分配方案.兩層可靠度指標分配算例初步驗證了本文方法的正確性與可行性,三層可靠度指標分配算例證明了本文方法的有效性.最後,以重量指標分配為例,簡要敘述了針對飛機頂層設計中設計指標協同分配的數學模型和求解思路
  15. 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

    探討了一種新的設計指標最優分配方法- -協同分配法,用於處理飛機頂層設計中的大規模設計指標最優分配問題.分析了飛機頂層設計中的設計指標最優分配特徵,據此給出了協同法的原理並建立了數學模型.協同法按設計指標分配關系將最優分配問題分解為主系統優化和子系統優化,主優化對子系統設計指標進行最優分配,子優化以最小化分配設計指標值與期望設計指標值之間的差異為目標,進行子系統最優設計,或對底層元件(如飛機翼梁、翼肋和翼盒等)進行設計指標最優分配,並把最優解信息反饋給主優化.主優化通過子優化最優解信息構成的一致性約束協調分配量,提高系統整體性能,並重新給出分配方案.主系統與子系統反復協調,直到得到設計指標最優分配方案.兩層可靠度指標分配算例初步驗證了本文方法的正確性與可行性,三層可靠度指標分配算例證明了本文方法的有效性.最後,以重量指標分配為例,簡要敘述了針對飛機頂層設計中設計指標協同分配的數學模型和求解思路
  16. Activates stack probes for every function call that requires storage for local variables

    為需要局部變量存儲的每個函數調用激活堆棧探測。
  17. Optional the number of bytes that local variables can occupy before a stack probe is activated

    (可選)在激活堆棧探測之前局部變量可以佔用的位元組數。
  18. Dependencies on uninitialized local variables

    未初始化的局部變量上的依賴項。
  19. Its local variables are instance variables, including the

    ,則其局部變量為「實例變量」 ,包括
  20. Because the entire body of the method is a single block, i can define and use local variables within the body without any problems

    因為整個方法是一個塊,所以我可以毫無問題地在正文中定義並且使用局部變量。
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