helicopter control system 中文意思是什麼

helicopter control system 解釋
直升機操縱系統
  • helicopter : n 直升機。vt 用直升機載送。 helicopter sb aboard the ship 用直升機把某人送到船上。vi 乘直升機。n ...
  • control : n 1 支配，管理，管制，統制，控制；監督。2 抑制（力）；壓制，節制，拘束；【農業】防治。3 檢查；核...
  • system : n 1 體系，系統；分類法；組織；設備，裝置。2 方式；方法；作業方法。3 制度；主義。4 次序，規律。5 ...
  1. The research and development of flight control system is not dissociable with simulation technology. simulation has become an important tool for successful development of flight control system of unmanned helicopter

    無人直升機飛行控制系統的研製已和模擬技術密不可分，模擬已成為無人直升機飛行控制系統研製成功的必要手段。
  2. Helicopter is hard to hover precisely for its bad stability. ordinarily, it is improved by flight control system, such like rotorcraft unmanned aerial vehicles which use bell bar or bell - hiller stabilizer bar. bell stabilizer bar, fixed across with teetering main rotor, consists of a bar and masses at two ends

    貝爾穩定桿由一桿與兩質量塊組成，它與貝爾直升機的蹺蹺板旋翼垂直交叉放置，這種旋翼裝置有助於加大角速度阻尼，改善貝爾直升機的穩定性，但同時也降低了操作性。
  3. Finally, the thesis developed 3d animation flight simulation platform for helicopter using opengl in visual c + +. and the 3d terrain and helicopter model are constructed. the simulation of two typical maneuver ( s maneuver flight and bopup - bopdown ) and terrain following shows that the fight control system of attack helicopter is improved by the realistic optical impact

    本文最後在vc環境下用opengl開發了直升機三維動畫模擬平臺，構造了三維地形和直升機模型，模擬了直升機做蛇形機動、急躍升急躍降、地形跟隨等機動飛行，通過逼真的視覺效果驗證了飛控系統的正確性。
  4. The modern unmanned helicopter flight control system is generally composed of the flight control computer, the servo driving mechanism, the sensor, and the ground monitor control system etc. in this thesis the research to the helicopter flight characteristics was conducted at first, and its flight dynamic model was preliminary discussed, especially the mathematic model under hung - stop condition was formulated and the algorithm of the controller was designed in detail

    現代無人直升機飛行控制系統一般由飛行控制計算機、伺服驅動機構、傳感器、地面監測控制等分系統組成。本文首先對直升機的飛行特性進行了研究，並且對飛行動力數學模型做了初步探討，尤其對在懸停狀態下的數學模型做了較為詳盡的公式推導和控制器的演算法設計。
  5. This paper focuses on the flight simulation research of flight control system of unmanned helicopter

    本文就是針對無人機飛行控制系統中飛行模擬這一環節進行研究的。
  6. After target is detected the on - board avionics suite in combination with the automatic control system of the helicopter solve the task of bringing the helicopter to the designated point and automatic firing of the weapons selected by the pilot

    當捕獲目標后，機上的自動控制系統與電子系統將解算任務數據，引導直升機飛向敵潛艇水域，並在飛行員指令準許下自動發射武器進行攻擊。
  7. The china helicopter research and development institute is the only professional scientific research organization for helicopters design, research and experiment. it is the leader of the chinas helicopter development in this industry. the xbrothers security and facility control system has been applied in its computer room

    中國直升機設計研究所是我國唯一一家專門從事直升機設計研究試驗工作的綜合性大型科研單位，在新型號和改進改型設計新技術攻關先進技術預研項目中，充當著中國直升機工業陣營中的「革命軍中馬前卒」 。
  8. Research on debugging strategy of comprehensive performance specifications for simulator of fire control system in armed helicopter

    武裝直升機火控系統模擬轉臺的綜合性能指標調試策略研究
  9. The flight control system of attack helicopter and the influence of disturbance during noe flight are studied in this dissertation. and the use of h robust control and dynamic inversion schemes in flight control system are discussed

    本文主要對貼地飛行時武裝直升機的飛行控制系統進行深入的研究和探索，討論了貼地飛行時氣流擾動對直升機系統的影響，研究了h _魯棒控制和動態逆控制在直升機飛控系統中的應用。
  10. Introduction to flight control system of small unmanned helicopter

    小型無人直升機自主控制系統介紹
  11. A design strategy based on state feedback and feedforward compensator for helicopter flight control system

    基於狀態反饋及前置補償策略的直升機飛控系統設計
  12. It is important to soft developing. the topic of the paper has been listed in the basic research project for national defence of the " tenth - five project " by the commission of science technology and industry for national defence. one is " distribution experimentation and test technology ", the other is " mathematic helicopter and test technology ". base on the research of literature of the world, we will research the technology of measurement and control system

    本文結合十五國防預研項目「分散式協同綜合虛擬試驗與測試技術」和個五航空預研項目「直升機飛行載荷全數字加載控制和數據採集技術」的研究，在分析了國內外研究現狀和技術發展趨勢的基礎上，對其共性的關鍵技術之一? ?系統開發支持平臺（通用測控平臺）技術展開了深入研究。
  13. Finally according to the performance of unmanned helicopter model, we designed the hardware and software of the servo control system based on a psd3234a mcu. also we built a test platform for the helicopter system

    最後根據無人直升機模型性能，在硬體和軟體上設計並實現了基於psd3234a單片機的舵機控制系統，搭建了一種小型無人直升機模型飛行控制實驗平臺。
  14. Along with development of tiltrotor vehicle ’ s research some theoretical productions have been appeared in some project ( aerodynamic behavior of rotor, kinetic behavior of rotor, rotor / wing aerodynamic interactions, etc. ). in order to carry on further research and experimentation of these project, national - defence science and technology helicopter rotor kinetic lab of our school begin to building tiltrotor model bench. base on need of this bench, this paper study / design pitch control system on it

    隨著對傾轉旋翼飛行器的深入研究，傾轉旋翼的氣動特性、動力學特性、旋翼/機身間的氣動干擾等課題方面已有一定的理論成果出現。為了對這些課題進行深入研究和試驗驗證，我校直升機旋翼動力學國防科技重點實驗室著手建造了傾轉旋翼模型實驗臺。
  15. Design of sliding mode control system for a feedback linearisable helicopter nonlinear model

    基於反饋線性化的直升機滑模控制系統設計
  16. In this paper involved several aspects about the inner and outer loops design for helicopter flight control system, maneuver flight simulation for helicopter, terrain following simulation and 3d animation flight simulation system designed with opengl

    主要的內容包括直升機飛行控制系統內外迴路設計、直升機機動飛行的模擬、地形跟隨的模擬以及opengl三維動畫模擬等方面的內容。
  17. This paper, in advantage of modern control theories, designed the pitch control system and the altitude holding system of the x armed helicopter, and present digital simulation, coupling analysis, sensitivity analysis, system performance analysis under different input and initial condition

    本文應用現代控制理論設計了某型武裝直升機的俯仰角控制系統和高度保持系統，並進行了數字模擬、耦合分析、飛行狀態變化對控制系統性能的影響分析，及在不同輸入初始條件下的系統性能分析。
  18. At the end of the dissertation, the fuzzy pd track tail controller is designed. the pd controller and controller of attitude angle are made up of flight control system of helicopter

    最後，本文設計了直升機模糊pd軌跡跟蹤控制器，與姿態角控制器相結合，完成了對整個飛行控制系統的設計。
  19. In view of the development of computer technology, it is feasible to simulate a helicopter, flight environment and control system designing by computer

    從計算機技術的發展情況來看，利用計算機模擬一架直升機、飛行環境以及控制系統設計是完全可能的。
  20. Using opengl and c + + builder6. 0, we developed a flight simulation software - lightdream1. 0. this software effectively implemented the real time flight monitoring function, flight simulation, path planning and displaying functions which satisfied the requirement of flight control system simulation of unmanned helicopter

    最後，採用borlandc + + builder6 . 0開發平臺和opengl圖形開發庫，開發完成了一套飛行模擬軟體? lightdream1 . 0 。該軟體有效地實現了直升機實時飛行監控、機動飛行科目模擬和軌跡規劃及顯示等功能，滿足了無人直升機飛行控制系統的模擬需求。
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