特技飛行術 的英文怎麼說

中文拼音 [tèjìfēihángshù]
特技飛行術 英文
aerobatics
  • 特 : Ⅰ形容詞（特殊; 超出一般） particular; special; exceptional; unusual Ⅱ副詞1 （特別） especially; v...
  • 技 : 名詞（技能; 本領） skill; ability; trick; technique
  • 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...
  • 行 : 行Ⅰ名詞1 （行列） line; row 2 （排行） seniority among brothers and sisters:你行幾? 我行三。where...
  • 術 : 術名詞1. （技藝; 技術; 學術） art; skill; technique 2. （方法; 策略） method; tactics 3. （姓氏） a surname
  • 特技 : 1 （特殊技能） stunt; trick2 [電影] special effects特技場景 trick scene; 特技飛行 aerobatics; aer...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  1. We also have made gift fans for 2000 year european football tournament, world aerobatics big prize competition around tailake, the eigth nationwide sports meet, the sixth china art festival and other great activities

    我廠曾為2000年歐洲足球錦標賽、環太湖世界特技飛行大獎賽、第八屆全國運動會、第六屆中國藝術節等重大活動製作禮品扇。
  2. On the basis of the research on the arresting behavior of the carrier aircraft, the arresting model of the continental rise aircraft as well as its motion analysis is presented in the paper

    本文對飛機著陸攔阻的技術進行了較深入的研究，主要是針對陸基飛機，借鑒艦載飛機的攔阻特性進行了攔阻鉤的建模及其運動學分析。
  3. The concept of irradiance signal - to - noise ratio ( snr ) on the target plane and the minimum of the irradiance that can be detected by the detector was taken as the beginning, combined with a thorough analysis of the spectrum radiating feature of the target and the sky background, the atmosphere conditions, spectral filtering and the influence that the various components in the system have on the target irradiance on the detector ' s target plane and the background irradiance snr, the equation of the flying bomb ' s effect range affected by the point of burst measuring system is made, and all related factors that have an impact on the effect range are analyzed as well

    從探測器靶面上輻照度信噪比的概念、探測器的可探測輻照度最小值出發，在詳細分析目標、天空背景的光譜輻射特性、大氣條件、光譜濾波技術以及系統各環節對探測器靶面上目標與背景輻照度信噪比的影響的基礎上，推導了炸點測量系統對爆炸的飛行彈體的作用距離方程，分析了影響作用距離的諸因素。
  4. The evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    敘述了20世紀50年代以來中國航天固體火箭推進技術的發展歷程，介紹了9種最具代表性的固體火箭發動機的技術特徵、研製過程、地面試驗和飛行情況，這些發動機分別應用於中國的探空火箭、運載火箭上面級和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展水平
  5. Abstract : the evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    文摘:敘述了20世紀50年代以來中國航天固體火箭推進技術的發展歷程，介紹了9種最具代表性的固體火箭發動機的技術特徵、研製過程、地面試驗和飛行情況，這些發動機分別應用於中國的探空火箭、運載火箭上面級和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展水平
  6. The simulation of " flight mission 3d visualization of the unmanned aerial vehicle ( uav ) " fully absorbs and applies current advanced 3d visualization theory, simulates the characteristics of true 3d volumetric display technique which are full - vision, multi - angle and can be observed by many persons at the same time and so on. it displays the process of flight according to mission of uav by the online of four computers

    「無人機任務飛行的三維可視化」模擬充分吸收和運用當前先進的三維可視化理論，盡可能的模擬真三維立體顯示技術的全視景、多角度、可供多人同時觀察等的特點，通過四臺計算機的聯機，在同一時刻從各個不同的角度來顯示無人機任務飛行的全過程。
  7. According to the measuremental data of the two ammunications, the anti - designed computation and analysis of aerodynamic characteristic, flight stability, exterior ballistic characteristic for the two ammunications are studied with the advanced methods of the exterior ballistics. using the monte calo algorithm, the statistic mathematical model about ammunication ' s intensity is established and the 1000 miter vertical target intensity and the fall intensity are discussed in detail for the two ammunications. the improval potential and the main technical approachs of these ammunication ' s exterior ballistic performances are presented by compositive optimal algorithm

    根據工廠對俄ak130艦炮彈藥的測繪數據，利用先進的外彈道數值分析方法對兩種彈藥的空氣動力特性、飛行穩定性特性、外彈道特徵量等進行了反設計計算分析；採用montecarlo方法，建立了艦炮彈藥密集度性能統計分析數學模型，對兩種彈藥的立靶密集度和地面密集度進行了詳細的計算分析；利用外彈道性能綜合優化設計方法對兩種彈藥的外彈道性能指標的改進潛力和主要技術途徑進行了分析。
  8. Article 130 the hong kong special administrative region shall be responsible on its own for matters of routine business and technical management of civil aviation, including the management of airports, the provision of air traffic services within the flight information region of the hong kong special administrative region, and the discharge of other responsibilities allocated to it under the regional air navigation procedures of the international civil aviation organization

    第一百三十條香港特別行政區自行負責民用航空的日常業務和技術管理，包括機場管理，在香港特別行政區飛行情報區內提供空中交通服務，和履行國際民用航空組織的區域性航行規劃程序所規定的其他職責。
  9. The hong kong special administrative region shall be responsible on its own for matters of routine business and technical management of civil aviation, including the management of airports, the provision of air traffic services within the flight information region of the hong kong special administrative region, and the discharge of other responsibilities allocated to it under the regional air navigation procedures of the international civil aviation organization

    香港特別行政區自行負責民用航空的日常業務和技術管理，包括機場管理，在香港特別行政區飛行情報區內提供空中交通服務，和履行國際民用航空組織的區域性航行規劃程序所規定的其他職責。
  10. The first man to walk on the moon noted that scientists must develop better onboard spacecraft technology and stronger protection shields from harmful space radiation before a manned flight to the red planet can be accomplished. " it will certainly be 20 years or more before that happens, " armstrong said during a global leadership forum

    據美聯社9月6日報道，阿姆斯特朗表示，在完成登陸火星的載人飛行之前，科學家們必須研發出更好的機載太空船技術以及更強的阻擋有害太空輻射的防護裝置。
  11. In consideration of the special mission characteristics and technical requirement of high altitude long endurance unmanned aerial vehicle, an authentic real - time and space - time windfield integrated model is accomplished to take atmosphere environment influences into account. at the same time, we should analyze the dynamics the uav encounters dispersedly, so the " finite scale " aircraft concept is quoted

    根據長航時無人機的特殊飛行任務特點和技術要求，在飛行試驗階段，有必要綜合考慮飛行環境中各種大氣干擾因素的影響，為無人機設計與模擬提供一個真實、適時的風場時空分佈模型。
  12. This thesis first states the characteristics of the equipments that have been adopted by the modern fighter and their basic technical performance. then an overall layered modular design for air combat simulation system is made utilizing system simulation technology and critical sub - systems have been mathematically modeled known as fighter body, propulsive system, flight control system, radar, fire control system, gun, air - air missile and avionics. after that a set of distributed air combat simulation system software is developed based on the scene graphics pc platform

    本文首先介紹了現代戰斗機空戰技術裝備及其基本技術性能特點；而後使用系統模擬技術，依據分層模塊化設計思想，制定了空戰模擬系統總體設計方案；之後根據目前技術狀況，建立了戰斗機機體、推進系統、飛控系統、雷達、火控系統、航炮、空空導彈、航電設備等戰斗機關鍵子系統數學模型；在此基礎上，根據總體設計方案，在基於pc的分佈互動式視景模擬平臺上開發了一套分散式空戰模擬系統軟體，實現了戰斗機互動式飛行模擬和分散式空戰模擬。
  13. The paper introduces the components and the technological characteristics of the unmanned air remote sensing vehicle, and expatiates the quick aquriring methods of three - dimensional building texture based on this system

    本文簡單介紹了無人駕駛飛行器低空遙感系統的組成、技術特點，並闡述了基於該系統的三維城市建築物紋理快速獲取方法。
  14. In this paper, the backward simulation was summarizd at home andabroad, the characteristics of shell nosing were introduced, the theory and scheme of backward simul - ation of shell nosing was constructed, the determined methods of the boundary conditions were put forward in backward simulation for the processes of shell nosing

    論述了推力矢量控制技術是提高空空導彈性能的核心技術，介紹了常用的三類推力矢量裝置，著重討論了燃氣舵式和擾流片式推矢裝置的特點、設計方法、性能及其優缺點.在此基礎上，研究了適用於氣動力/推力矢量復合控制的變結構控制系統及其開關函數的切換條件和飛行控制系統框圖.最後綜述了推力矢量裝置在第四代空空導彈上的應用情況
  15. Precision transmission device is one kind of the key fundamental components, which are extensively applied to many industry fields including robot industry, machine industry, instrument industry etc. with the development of information technology and space navigation technology, especially the micro - miniaturization, speediness and automation of satellite communication, scouting the flying project, remote sensing and measuring and astronomic observation antenna system, more hard requirements are demanded on precision transmission

    精密傳動是一種重要的基礎性零部件，在機器人、機床、儀器儀表等工業領域有著廣泛的應用。隨著信息和宇航科學技術的發展，特別是衛星通信、飛行目標跟蹤與攔截、遙感與遙測、天文觀察等天線系統的微小型化、快速化及自動化，對精密傳動提出了更高的要求。
  16. The aircraft in the future must have the ability of lightweight, small size and low power consumption. the smart skin compositing the devices made by mems technology which have self - sensing and self - adapt controlling functions meets with the requirement mentioned above

    未來航空飛行器要求微型器件具有質量輕、體積小和功耗低等特點，採用mems技術製造的由微型器件陣列組成的具有自檢測、自適應控制功能的靈巧蒙皮可以很好地滿足上述要求。
  17. With the development of simulation - technology and virtual reality, virtual prototype based on system simulation, flight dynamics, electronic technique, autocontrol theory and cad / cam has been more and more widely applied to the military rehearsal and the design and manufactural process of major weapon system

    隨著模擬技術特別是虛擬現實技術的發展，以系統模擬、飛行動力學、電子技術、自動控制理論以及cad cam技術等為基礎的虛擬樣機技術在大型武器系統的研製以及軍事演習等方面的應用愈加的成熟起來。
  18. It ' s a driving force and also a challenge to control in both theory and technology due to the more and more severe specifications imposing on it. a variety control theory have been developed, however, with limited performance in practical applications, especially in term of the relatively lower response speed when used in those machines which run fast. therefore, it is necessary to develop a new self - tuning algorithm for fast running plant of uncertainty so as to set theoretical base for controller design

    在科技飛速發展的今天，各種新設備、新工藝的出現促進了控制理論的發展，同時也對控制技術提出了越來越高的要求，雖然已有許多旨在提高控制性能的不同的控制理論，但由於其各自的局限性，在應用中仍然存在許多問題，特別是對于運行速度較快的機械設備等，其響應時間往往不能達到要求，因此，有必要開發一種新型、快速、能夠適應快速運行或變化的對象或過程的自調節演算法，以為控制器的開發作好理論支持。
  19. It was analyzed about the problems of space vehicle flight control, the development of space vehicles, the design aim and main characteristic of flight control systems of varied space vehicles, the main design requirement of flight control system of reusable space vehicles, the key technology which have to be resolved in flying control law design and flight control system design

    摘要分析了空間飛行器飛行控制系統要解決的問題，空間飛行器的發展過程，各類空間飛行器飛行控制系統設計目的和主要特點，可重復使用的發射飛行器飛控系統的主要設計要求，在設計要求的確定，飛行控制律設計和飛行控制系統設計中要解決的關鍵技術。
  20. This thesis presents an aircraft health monitoring laboratory design scheme. based on virtual instrument technique, the laboratory is constructed with basic hardware and varied developed signal processing, diagnosis, and health monitoring computer programs. this scheme makes it flexible, economical, and time - saved for various kinds of research

    本文提出了一個飛行器健康監控技術實驗室方案，主要特點是基於虛擬儀器技術，通過配備基本的硬體和開發各類信號處理、故障診斷、健康監控軟體來構建實驗室，從而可以快速、靈活、經濟地開展各種相關研究。
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