飛針型 的英文怎麼說
中文拼音 [fēizhēnxíng]
飛針型
英文
flying probe-
The enterprise flytex koch sauer gmbh co buoyancy membranes kg is well - known and engaged not only in rimsting, but also in the specialized industries of its sphere of activity, with boxes, airships, assembly details and at the same time with ballonet, balloon and standard programme a competent partner
Flytex koch sauer gmbh co buoyancy membranes kg是一家現代化的、可靠的專門產品供應商，這家供應商從事系留氣球，球形玻璃瓶、氣球，副氣囊，裝配細節，充氣光電管，外罩、外殼，飛船、飛艇，薄膜、膜片，程序、節目，船舶、船，切削刃、刀刃，鉛垂、探針，特殊成型，標準程序的製造、銷售。Our company owns the knitting dyeing factory, the electronic toys factory and the hardware products factory, mainly do the business relating to sell " shen qi wei " micro radio control racing car ( hottest ), 1 / 10 scale radio control 4wd high performance racing car ( new ), radio control electric plane ( hottest ), mini electric duplicator, light control gifts, sonic control dolls, little pals, jumping ball in china and i / e all kinds of products
本公司擁有針織染整廠、電子玩具廠和五金製品廠等一條龍出口生產加工基地，主要經營「神奇威」微型遙控車（熱） 、 1 / 10新數字比例遙控車（新） 、遙控飛機（熱） 、遙控玩具、光控禮品、電動迷你影印機、電動玩具、電子跳跳球、電子玩具、塑料玩具、聲控娃娃，玩具設計加工及各種進出口貿易。In this system, we use a computer model to simulate the true aeromodelling ' s wing, and then we simulate the state of aeromodelling ' s wing under the real flying conditions by computer. moreover, we simulate two fault - models for wing ' s model, and then we get the state ' s date of wing ' s model structure when the two faults are happening
在建立這個健康監控系統中我們採用在計算機上建立的模型來模擬航模飛機的機翼並在計算機上模擬了飛機在真實情況下的飛行受力狀態，接著我們在計算機上針對機翼模型模擬了二個故障，並計算出了在這二個故障發生時機翼結構的受力狀況。A certain institute wants to develop a universal semi - physical simulator for certain avionic system. based on this background, this paper discusses the analysis, modeling, design and implementation of the universal semi - physical simulator detailedly
為此，某飛機設計研究所針對某型號飛機航電系統的研製提出了航電系統通用半實物模擬設備的研製要求。The thesis roots in the item supported by " fifteen " aviation funds, - new type aeronautic linear dc motor ( ldcm ), study its classes characteristics and work principle, mainly researches the drive and control technique of aeronautic linear dc step motor ( ldcsm ) using in emergency discharging oil valve on airplane
本文源於「十五」航空支撐基金項目-新型航空用直線直流電動機。論文研究了直線直流電動機的分類、特點及其工作原理，重點針對飛機應急放油閥用航空直線直流步進電動機驅動控制技術進行了研究。The thesis analysed the chief technique problems and designed the solution algorithms, proposed measures of the software fault tolerance techniques suitable for the hardware platform of the robotic system on the base of studying the two key techniques - eddi and cfcss. first, the thesis has done the analysis in theory for the chief technique problems including basic block partition, software signature instructions generation, shadow instructions generation and instructions scheduling, proposed the algorithms suitable for the target platform. then, the thesis introduces the design process of the software fault tolerance
本文在研究了sihft的兩項關鍵技術?復制簽名檢錯技術和軟體簽名控制流檢錯技術的基礎上，針對小型智能飛行機器人系統的硬體平臺，對軟體檢錯技術的關鍵問題進行了分析並給出了解決問題的演算法，提出了適于小型智能飛行機器人硬體平臺的軟體檢錯技術方案。Focusing on the advance research of the flight control computer system of some type of a high altitude, long endurance unmanned aerial vehicles, this paper analyzes and research its staicture in techniques of redundancy fault - tolerance
本文針對某型號預研高空長航時無人機飛行控制計算機系統的可靠性要求，運用冗餘容錯技術對其進行了設計研究。The present study was aimed to develop a solid - culture - based technology for easy and cheap propagation of p. delphacis f95129 inocula using small grains as substrate for fungal growth. sporulation capacity and timing pattern were relied upon to evaluate culture quality and identify potential factors to affect the quality. infectivity or virulence of inocula derived from the culture was assayed against the green peach aphid, myzus persicae ( sulzer ), based on time - dose - mortality modeling
針對這一普遍性的技術難題，本研究以飛虱蟲癘霉f95129菌株為對象，以黍米、粟米為基本材料，探索建立簡便易行的侵染體繁殖技術體系，並對培養物進行了產孢潛能及其影響因子的評價以及針對桃蚜（ myzuspersicae （ sulzer ） ）的侵染性測定和時間?劑量?死亡率模型模擬。Aerospace - airframe needle track roller, yoke type, single - row, sealed - inch series
航空航天.飛機結構用軛型單列密封的滾針滾道式滾子.英制系列The main research work of the thesis is summarized as follows : 1. the improved fuzzy logic control method the phenomenon of steady - state errors and flutter exists in the traditional fuzzy controller. an improved fuzzy controller without quantilizing is presented
地形跟隨飛行控制律設計針對某型飛機應用控制航跡角法和控製法向加速度法對不同的反饋信號分別設計了pi控制器和模糊控制器，並做了模擬比較與魯棒性驗證。According to the requirements of propeller aerocraft model test in wind tunnel, specifications of the driven motor is presented by aerodynamic analysis, and a short - term operated high power density three - phase induction motor is developed with reasonably designing the motor, such as electromagnetism load, heat checkout and high - efficiency heat exchanger
摘要針對螺旋槳飛機模型帶動力風洞實驗要求，通過氣動性能分析提出驅動電機的技術指標，在滿足結構約束的條件下，通過合理設計電機的電磁負荷、校核發熱、採用高效冷卻裝置等，研製出短時工作制高功率密度三相異步電機。According to the feature model proposed by the author, prototype system for integer panel is developed on pc
另外，根據全息特徵模型的理論，編寫了針對飛機整體壁板類零件的設計原型系統。It is the propose of this paper to develop a method to reduce the noise level of ma60 apu without more weighting and other infection on airplane. to accomplish this object, a new type of micro perforated absorber is used
針對新舟60飛機apu本身的結構和環境特性，我們採用一種新興的環保型消聲材料-微穿孔板為上要吸聲結構完成降噪設計。The application background of thrust vectoring technology on aircraft and its advantages are analyzed. the main characteristics of some type of vectoring nozzles are discussed, the expression of thrust vectoring force and moment are set up. then, the nonlinear motion equations of aircraft with three axes of thrust vectoring are deduced
本文主要針對推力矢量飛機非線性飛行控制的理論和應用問題進行了一定的探索和研究，進行的主要工作有： 1 、研究了推力矢量在飛機上的應用背景和收益，分析了現有推力矢量噴管的主要形式和特點，給出了推力矢量力、力矩的數學模型，並在此基礎上推導了帶三軸推力矢量飛機的非線性運動方程，為控制律的設計奠定基礎。The maintenance program must be prepared before operating for the new type aircraft. it is the base and frame for airlines to determine preparatory maintenance policy and maintenance document, and is one of the based document insuring aircraft airworthiness
每一種新型飛機投入使用前必須制訂一份維修大綱，它是航空公司控制其初始維修方針，制訂維修方案的基礎和框架，是保證飛機持續適航的基本文件之一。A miniature electromagnetic yoke was developed for the inspection and maintenance of the complex components of planes
摘要針對航空維修中飛機復雜構件檢測維護的特點，研製了適用於外場作業的微型電磁軛。The research on flight plan conflict probe ( fpcp ) : in the phase of flight plan preparation, the planning controller of air force used to spend half time of each day to draw the routes on the maps and then probe the conflicts between them, for the flight routes are quite irregular and more possible to cause conflicts with other training flights or civil aviation flights. the fpcp model studied here is one of the innovation applied in mrd2k - jh, it can automatically probe all the potential conflicts between flight plans. this model uses 4 - d conflict probing rules to analyze all the route information of flight plans, the detected conflicts ( route points or segments ) can be useful for assisting the planning controller to amend the conflicted plans and re - probe the conflicts
飛行計劃沖突預調配研究：針對軍航管制工作中飛行計劃機動多變造成飛行沖突多、沖突探測繁、手工調配難的情況，介紹了mrd2k ? jh系統中採用的一項創新之處? ?飛行計劃準備階段自動化的四維沖突探測模型，按照飛行安全間隔對各飛行計劃的所經航線數據進行潛在沖突分析，探測出預沖突航路點或沖突航線段，代替了軍航管制員原來在地圖上手工測畫的重復性勞動，該項功能幫助管制員及時發現飛行計劃之間存在的潛在沖突以方便進行調配再探測，不僅極大提高了工作效率，更避免了人為可能造成的失誤，確保了飛行的安全。Two new algorithms, adaptive model and adaptive interacting multiple model, are presented in this paper with respect to the maneuvering trajectory characteristics of anti - ship cruisle missiles
針對比例制導的飛航式反艦導彈彈道的特點和機動特徵，提出了跟蹤此類目標的兩種新演算法? ?基於自適應模型的演算法和基於自適應交互多模型的演算法。Planes is characterized by complex structure and involving in much factors in a air war, this paper establish two - level structure model based on the characteristics of planes, and calculate the weight of each plane ' s qualities by ahp, and present a approach to validate the consistency of weight
針對飛機結構復雜和空戰涉及因素較多等特點，建立了兩級遞階結構模型，利用層次分析法計算了飛機空-空作戰中各品質因素的權值，並給出了進行一致性檢驗的方法。Development of an antiradiation sam, most likely intended to target awacs aircraft and standoff jamming platforms
研發一種反輻射面對空導彈，最有可能是針對awacs飛機和抵銷型干擾平臺。分享友人