army research and development 中文意思是什麼

army research and development 解釋
陸軍研究與發展
  • army : n. 1. 陸軍；軍隊。2. 軍；集團軍；兵團；野戰軍。3. 大群；團體。
  • research : n. 1. 仔細搜索 （for, after）。2. 〈常 pl. 〉研究，調查，探測；追究。vt. ,vi. 追究；調查，研究 （sth. , into sth. ）。
  • and : n. 1. 附加條件。2. 〈常 pl. 〉附加細節。
  • development : n. 1. 發展，發達；進化。2. 展開；擴充；開發。3. 發達物，新事物，發展階段。4. 【生物學】發育（史）；【軍，數】展開；【攝影】顯影，顯像；【音樂】展開（部）；研製，研製成果。
  1. U. s. army ordnance research and development service

    美國陸軍軍品研究與發展服務處
  2. And the architecture is born of oop and coordinate the class inheritance way to implement the workflow inheritance architecture. it made the workflow model have the reusing and polymorphism as the class. to the purpose of army automatic approving, the main contents of research in this dissertation are as follows : 1 ) analyze the current status and the shortage of workflow development by

    特別給出dbflow工作流引擎支持的工作流模型繼承體系，該體系來源於面向對象的思想，結合類繼承的方式，實現工作流模型的繼承機制，從而使工作流模型能象類一樣具有重用性，甚至多態性。
  3. In order to provide a basic and effective practical engineering tool for handling quality planning, analysing and evaluating, which is needed hi helicopter prototype development, this research work is launched on the fundation of comprehending the new aeronautical standard of united states army - ads - 33, and has obtained the achievements as following : ( 1 ) performance definition of pcs according to the criteria requirements for an explicit helicopter, beginning at analysis of its missions. ( 2 ) establishment of a helicopter attitude controller, which can meet the criteria requirements, by using the technology of adaptive neural network model - inverse control ; implementation of two response types ( rts ) and two control modes ; evaluation of quantitative parameters according to the ads - 33. ( 3 ) establishment of a helicopter trajectory contoller based on the attitude controller ; simulations of mission task elements ( mtes ) and evaluation of handling quality

    為了給型號研製中飛行品質的規劃、分析和評價提供基本的、有效的工程實用工具，本課題在充分消化理解美軍新航標ads - 33的基礎上，作了以下工作： （ 1 ）針對具體直升機，從任務分析入手，根據規范要求確定對飛控系統的要求； （ 2 ）應用自適應神經網路模型逆控制技術，構造了能夠滿足飛行品質要求的直升機姿態控制器，實現了兩種響應型式、兩種控制模式，並根據ads - 33進行了定量指標評估； （ 3 ）在姿態控制器的基礎上，構造了軌跡跟蹤器，進行了任務科目基元模擬和飛行品質評估。
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