最後試航 的英文怎麼說
中文拼音 [zuìhòushìháng]
最後試航
英文
a shakedown voyage flight trial etc-
This phrase is borrowed from the aeronautics flight testing industry of the 1950 ’ s, when pilots flew increasingly faster, or “ pushing the envelope ”, eventually breaking through the sound barrier and further
這一個片語從1950年代的航空學飛行測試業被借，當飛行員逐漸地更快速地飛了的時候，或"推到極限" ，最後突破健全的障礙和比較遠的。Lastly but not the least, this paper proposes not only the existing problem of the quality assessment system of aids to navigation but also the suggestion of continually adjusting the index with trying out it and accordingly programming its relative software
最後，論文中也提出了航標質量考核指標體系中存在的問題，提出了通過試行航標處的航標質量考核指標體系來不斷調整指標的建議，以及針對海區的航標質量考核指標體系，建立相應的考核管理軟體的建議。Subsequently, the communication of wireless is introduced as well as the key points of receiver ’ s rf front end. then, the design methods of receiver with high linearity and high dynamic range are recommended too. also, the blue print of the receiver, the achievement of function guide line and the problems in real debugging are discussed in detail
本文先介紹了當代無線電導航的狀況以及發展趨勢和無線電的傳播，然後對接收機射頻前端的關鍵技術指標進行了深入分析，還介紹了系統在大動態范圍，高線性實現的一些設計方法，之後詳述了本項目採用的方案、具體功能指標的實現以及在設計與實現中應該注意的問題，最後給出系統的測試結果。It is found that this system can provide basic mapping functions such as handling interior, relative, and absolute orientations, and maintains the perspective relation of the stereo - pair during the mapping process
測試區為臺南市東區虎尾寮附近地區之立體航照像對及地面控制點，最後以立體觀測重新檢測控制點座標。The main tasks of this thesis are : discussing the dead - reckoning theory of doppler velocity log and compass, decreasing location error methods, emulating several ship tracks ; discussing several aspects influencing the velocity precision of doppler velocity log ; in a pool trial, processing the trial data and achieving some conclusions
本論文主要研究工作包括：對羅經和多普勒計程儀推算輔助導航系統的工作原理，及減小定位誤差的兩種方法和幾種軌跡進行了研究；對影響多普勒計程儀測速誤差的各個方面進行了綜述；最後對多普勒計程儀水池試驗的數據進行了處理，得出所要結論。And the last, some sea trial results show that the match among the main engine and propeller is slightly heavy for the real vessel construction. although the reasons are very complex, most of them can be resolved by the method of propeller trailing edge modification. because of lack of guidance in theory, the actual quantities of modification were very difficult to decided and lots of quarrels may be raised between the shipyard and the owner before
最後，針對實際船舶建造過程中，部分船舶的試航結果表現出來的機槳匹配稍重問題，雖原因比較復雜，但絕大部分可以採用螺旋槳隨邊修正的方法解決，因為沒有理論數據給予指導，很容易引起爭議，在具體修正的數量上較難卻定，其修正後的螺旋槳工況更難準確預報。In the end of the paper, the lqt based on ga is applied to design the flight control system of rss uavs. the intensive simulation verified the validity of our research
最後，應用基於遺傳演算法的線性二次型跟蹤器技術對放寬航向靜穩定性無人機的飛行控制系統進行設計，試驗結果驗證了研究成果的有效性。Finally, the module debug and task implement are mainly carried out using serial port and network in host ’ s environment. these are supported for further data management in reality of micro satellite
最後主要利用串口和網口結合主機進行任務模塊程序的編寫和功能模塊調試，這些工作對最終進行微小衛星航天應用打下一定的基礎。At last, some practical navigation data in hong kong are processed by algorithm improved and woleson ' s. it is proved by the results of experiments that new algorithm not only decreases the number of characteristic point, but also predigests curve matching algorithm. the new algorithm makes full use of curve characteristic information in matching process
最後，利用香港地區的實際導航數據，分別採用改進演算法和woleson演算法進行計算，分析試驗結果，證明改進后的演算法不但降低了對特徵點的依賴，而且在匹配中充分利用了曲線特徵信息，簡化了曲線匹配演算法。The paper firstly analyzes the characteristics and demands of an electronic aeroengine controller, as a result, the design scheme of a primary module, which is based on dsp and can, is proposed for an electronic aeroengine controller. then, according to this scheme, a primary module is implemented by hardware design and software development. finally, a wpa aeroengine mathematical model is used to construct a matter - in - loop simulation system, with which a series of control system experiments are accomplished
論文首先分析了航空發動機電子控制器的特點，提出基於dsp帶can總線介面的航空發動機電子控制器核心模塊的設計方案；然後根據此方案，通過硬體電路的設計和軟體開發，實現了該核心模塊；最後利用渦噴a發動機的數學模型構成一個實物在迴路模擬試驗系統，並完成了模擬試驗。He will be assigned to work in the air traffic control centre where the work nature is less time - critical. prior to performing solo duties, he will be required to undergo intensive simulator as well as on - the - job training under the supervision of qualified instructors before being checked out. thereafter, his work will be closely monitored by his supervisors
他將被調至航空交通控制中心，處理時間緊迫性較低的工作，他將需要接受密集的模擬訓練，並且在合資格的導師監督下，在實際環境下接受訓練，最後經過嚴格的考試才會再次單獨工作，而其主管亦會密切注意其表現。Finally, according to the mode of two - roles in teaching, which should give play to teachers " leading role and also fully reflect students " cognitive subject. and on the basis of following the course teaching design principle of the network, carry on the website design and develop of the course of " hydraulics & pneumatics ". firstly utilize frontpage2000 of the developing instrument of web page to designed and develops website ' s overall style, the interface, style of navigating and studying the supplementary function that courses need ; then utilize jsp and javabeans discreteness technology to carry on real procedure making, in order to reach the function of various kinds of websites and teaching purpose, such as the operation to backstage supporter ' s data base, realize website ' s registration and log on, realize the search and study offered for studying and is tracking the studying ; then imbed the network packs in the corresponding web page, and regulate the linking of these web pages, make it reach anticipated request, and debug running in campus network
最後，按照雙主教學模式（即發揮教師的主導作用和學生的認知主體作用） ，並且在遵循網路課程教學設計原則的基礎上，進行「液壓與氣壓傳動」課程的網站設計與開發：利用網頁開發工具frontpage2000進行網站總體風格、界面、導航風格以及學習課程所需輔助功能的設計與開發；利用jsp及其， tavabeans組件技術進行實際的程序開發，以達到對后臺數據庫的操作、實現網站注冊及登錄、實現為學習提供的搜索和學習跟蹤等等各種網站功能及教學目的；把網路打包好的課件嵌入相應的網頁中，並對這些網頁的鏈接進行調節，使其達到預期的要求，並在校園網上進行調試運行通過。Prior to its implementation, extensive trials on cda involving aircraft from cathay pacific airways limited initially and all other airlines in the final phase have been conducted with successful results
民航處在決定實施持續降落模式前曾進行廣泛測試，最初只涉及國泰航空有限公司的飛機，最後階段則獲其他所有航空公司飛機參與，測試結果成功。Based on the architecture of the as / 400 server, section 3 also puts forward based develop solution of described the construction of the flight arrangement information management system develop for both of hardware platform, software platform and development tools. section 4 discussed the implementation of the applications software, in details. section 4 also particularly introduces the design and realization of the flight data input module, the flight aided arrangement module, the sold seats computation module, the important data maintain module and common forms generation module
本文首先介紹了管理信息系統的基本概念；然後分析了航班調度信息管理系統的功能需求，比較了其幾種可行的實現方案，提出了以as / 400為服務器的系統總體開發方案，論述了硬體設計選擇和軟體總體設計和模塊劃分；接著，介紹了軟體開發環境和工具，並對航班數據錄入、航班輔助調整、銷售座位數計算、重要數據維護、常用報表生成等各個軟體模塊的設計與實現進行了詳細的介紹；最後，說明了對開發所得系統進行測試的結果以及今後改進的構想。Finally, combining algorithm flow - chart of the sins, all work realizes test and validation of the hardware circuit system
最後，結合捷聯式慣性導航系統演算法流程，對硬體電路系統進行了測試驗證，並給出了測試結果。分享友人