飛機次系統 的英文怎麼說

中文拼音 [fēijīcìxìtǒng]
飛機次系統 英文
aircraft subsystem
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 機 : machineengine
  • 次 : Ⅰ名詞1 （次序; 等第） order; sequence 2 [書面語] （出外遠行時停留的處所） stopping place on a jou...
  • 系 : 系動詞（打結; 扣） tie; fasten; do up; button up
  • 統 : Ⅰ名詞1 （事物間連續的關系） interconnected system 2 （衣服等的筒狀部分） any tube shaped part of ...
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 系統 : 1. （按一定關系組成的同類事物） system 2. （有條理的;有系統的） systematic
  1. The paper describes the work as follows. first, based on the knowledge of collapsar technics, this paper analyzes the characteristic of optical fiber collaperser machine software system and hardware structure, a p8 system and it ' s development kit has been installed first in china, and the hardware system of the optical fiber preparation collapsar has been designed and debugged

    本文主要做了以下幾方面工作：首先，在了解光纖預制棒熔縮機工藝的基礎上，剖析了長飛光纖光纜有限公司的光纖預制棒熔縮機的軟、硬體的特性，在國內首次組裝了p8及開發系統，設計出光纖預制棒熔縮機的硬體系統，並作了調試。
  2. Firstly discussing basic type of computer redundant structure and characteristic of the systems, the self - monitoring dual redundancy computer systems is brought forward as the design scheme for the required flight control computer system. the redundant structure is researched about reliability by using markor model and is carefully designed

    首先分析了計算機冗餘結構的基本類型以及本次設計的要求特點，選擇了自監控二冗餘飛行控制計算機系統的設計方案，運用馬爾科夫模型對此冗餘系統的可靠性進行了計算研究，並且對此冗餘結構進行了詳細地描述及設計。
  3. Secondly, the development of aircraft icing avoidance technique, namely, the design idea, composing and function of smart icing system are introduced

    其次，介紹了飛機容冰技術的發展方向，即智能防冰系統的設計思想、組成及功能。
  4. The latest development of elmc, which is composed of distribution power center unit ( dpcu ) and electrical remote terminal ( ert ), is generalized in the paper. elmc scheme is presented according to the characteristic of avionics and the request of fault tolerant electrical power system ( ftep ). ftep structure based on 270v direct current is then designed to realize the demonstration of dpcu

    本文首先分析了elmc在國內外研究發展狀況，並依據航空電子系統特點和容錯供電要求，提出了由配電中心和控制中心組成的elmc的總體方案；完成了270v高壓直流供電的飛機容錯供電系統方案的設計，實現了供電系統中二次配電方案的控制與管理的模擬演示。
  5. Secondly, towed system is considered as many rigid body systems. according to research approaches of many rigid body systematic dynamics, the towed systematic engagement calculating models is derived ; according to actual course of the towed flight, deriving mathematics model of the course of taking off and towed flight of the towing plane and of carrier rocket, and corresponding parameter calculate models

    其次將牽引系統作為多剛體系統宋考慮，根據多剛體系統動力學研究方法，建立牽引系統約束方程，由此推導出約束力計算公式；根據牽引飛行實際過程，推導出載機、運載器在起飛階段，巡航飛行階段的數學模型，以及相應的參數計算模型。
  6. It is concluded that in order to achieve the ultimate goal of manufacturing excellence, philips dap zhuhai shall be changed as a learning organization by strategic synergy, and keep systematic, balanced improvement for building up an organic structure from the chaos

    文章提出，珠海飛利浦必須要將企業培養成學習型的組織、在戰略的層次協同相關工作，于混沌的環境中開展系統、平衡的改進，形成高度秩序化的有機結構，才能最終達到卓越製造的目標。
  7. 3. the project using ins / gps system data to estimate the angle of attack and sideslip is brought forward first. this project using the ins / gps system data, such as acceleration and velocity signal, and others signals of the aircraft, such as gyros and the mathematic models, to estimate virtual signal

    首次採用ins gps系統數據來估計迎角和側滑角傳感器參數原理和方法，利用ins gps系統測量的地速和總加速度信號結合飛機其他傳感器和數學模型估計得到了迎角和側滑角傳感器的虛擬信號，該種方法具有很好的實時性。
  8. The system is designed to search, track, process and display ssr equipped aircraft within an airspace of 32 nautical miles in range and 15, 000 feet in elevation

    這套系統可搜尋、追蹤、處理和展示裝有二次監察雷達應答器的飛機及其飛行資料，覆蓋范圍達３ ２海里，覆蓋高度則達１ ５ ０ ０ ０英尺。
  9. Aeronautical static inverter ( asi ) is a kind of static converting device, which converts the dc ( 27v / 270v ) in the main power of aircraft into ac of constant - voltage and constant frequency by means of power semiconductor devices. with the development of the aircraft, all the electric equipment on the plane requires the power supply system with better performance

    航空靜止變流器（ asi ? aeronauticalstaticinverter ）是航空電源系統的二次電源，其作用是將飛機主電源直流電27v或270vdc變換成恆壓恆頻單相115v 400hz ，單相36v 400hz ，三相115v 200v ，或三相36v交流電，供飛機上負載使用。
  10. " the cnsatm has immense benefits in enabling aircraft to operate more frequently within their most optimum flight envelop, while minimising airspace constraints, and reducing traffic congestion. it also commensurates with achieving a marked increase in flight safety

    該系統不但能容讓航機在最佳的飛行狀態范圍增加飛行次數，把空域限制減至最少，紓緩航空交通擠塞，而且更可顯著提高飛行安全。
  11. 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。
  12. The electro - hydraulic proportional control law is given. the laws of tracking control of displacement and speed of aircraft as well as tracking control of angle and angular speed of belt wheel are designed by means of state feedback linearization and quadratic performance index linear optimal control method. the robustness of the designed systems is analyzed, and arresting processes are simulated

    給出了電液比例控制規律；利用狀態反饋線性化及二次型性能指標線性最優控制方法分別設計了系統跟蹤控制飛機位移與速度以及跟蹤控制帶輪轉角與角速度的非線性控制規律；對所設計的攔阻系統進行了魯棒性分析及攔阻過程模擬，模擬結果表明，通過選取適當比例系數或控制權系數，兩種控制系統的控制效果及魯棒特性均優于新型飛機攔阻系統。
  13. In ccs ' c3x - ' c4x compile environment, using composite programming method of c and assemble language, the author debugs each port of the hardware circuit system, analyses interrupts mechanism and bootloader mechanism of the dsp, develops the system of generating flight orbit data

    其次，在ccs ' c3x - ' c4x編譯環境下，採用c語言和匯編語言混合編程的方式，初調了硬體電路系統的各個埠，分析了dsp晶元的中斷和bootloader機制，開發了飛行軌跡數據生成系統。
  14. The problems identified during this exercise will need resolution, to include updating aep, better coordination of unified incident command system, closely monitoring memphis fire training in dealing with response to aviation incidents, and station # 33 ( arff ) training to better understand safe and efficient use of apparatus in emergency situations

    在此次演習中觀察結果到的問題將需要解決，包括更新的機場應急計劃，更好的統一事故指揮系統的協調，進一步督導孟菲斯消防對于航空事故反應的培訓，以及加強對第33小隊（飛機救援消防）的培訓，使其更好的了解緊急狀況下對于器材安全而高效的使用。
  15. The design of aircraft cockpit, which acts as the man - machine interactive interface is of great research value. the author utilizing advanced cad technology, combining the intersecting knowledge with man - machine engineering, robotics, aero - human - engineering, etc, has exploited corresponding modules, such as the simulation of pilot manipulation, vision checkout, vision simulation, accessibility calculation, manipulation force calculation, and established a set of subsystem of aircraft - cockpit - design on the platform of catia

    本文利用先進的計算機輔助設計（ cad ）手段，結合人機工程學、機器人學、航空人體工程學等邊緣交叉學科知識，在catia平臺上，利用其二次開發語言vbscript ，實現了相應的飛行員操縱動作模擬、視界檢查、視覺模擬、可達性計算和操縱力計算等功能，初步建立起一套飛機座艙設計cad子系統。
  16. Secondly, after analysis of the task management ' s situation and abuse in the item management section, yield section and design section in xi ' fei company, several methods to optimize an enterprise ' s task management are put forward under the guidance of resolving problem one by one, such as defining the task in detail and developing a computer aided system of task management. and the operating theory of the task management is designed based upon its basic flow

    其次，在分析西飛公司的項目管理處、設計處與生產處的任務管理的現狀及弊端的基礎上，應用針對問題逐個解決的優化思路，提出了優化企業任務管理的幾點方法，如細化任務內容，建立一套計算機輔助任務管理系統；並且基於任務管理基本流程設計了任務管理的工作原理。
  17. In the surveillance system of cns / atm, secondary surveillance radar ( ssr ) is used in busy air space, and automatic dependent surveillance ( ads ) is used in other air spaces. ssr and ads can also be integrated. and ads can improve the efficiency of air space in the areas of ocean and desert where there is less flight route and large separation between aircrafts

    在新航行系統的監視系統中，主要發展雷達監視和自動相關監視，在繁忙空域採用二次雷達監視，其它空域採用自動相關監視，並且可以實現二者的數據耦合；通過自動相關監視，可以克服海洋、荒漠空域航線少，飛機間隔大的缺點，提高空域利用率。
  18. Building the prototype data integration system of civil aircraft, introducing mediated structure of this system. furthermore, information of structure, class, interface of each layer is described also. the work of this paper will build the infrastructure for developing perfect data integration system of civil aircraft

    3 .藉助web服務的服務思想，運用web服務相關技術建立民用飛機多數據源集成原型系統，介紹了該原型系統所採用的中間件系統體系結構，分別描述了原型系統中不同層次的結構、類、介面信息以及該系統的相關信息。
  19. The rdpds processes the radar data from various primary and secondary radars to present the aircraft position and its related information, e. g. aircraft callsign, altitude, ground speed, aircraft category, etc. on the radar display

    雷達數據處理及顯示系統可以處理來自不同的一次及二次雷達的數據，然後在屏幕上顯示航機的位置及其有關的資料，包括航機的代號、高度、速度、飛機種類等。
  20. Taking the soft ? sensing of oxygen content in flue gas, unburned carbon content in fly ash and coal load in ball mill as examples, we emphatically analyze the current status, modeling method of their soft ? sensing and the secondary variable selection in the soft ? sensing ; and also summarize some other thermal parameter soft ? sensing techniques in our country, which is a guidance for the development of the thermal parameter soft ? sensing technique in power plant, and has some value for the optimization of thermal control systems

    以煙氣含氧量、飛灰含炭量、球磨機負荷為例，著重分析和總結了其測量的現狀、軟測量建模方法和二次變量的選取，並概括了國內現有的其他熱工參數軟測量技術，對火電廠熱工參數軟測量技術的發展具有一定的指導意義，對熱工控制系統的優化具有一定的參考價值。
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