stability and control aircraft 中文意思是什麼

stability and control aircraft 解釋
安定性與操縱性研究機
  • stability : n. 1. 穩定,穩定性,穩度。2. (船等的)復原力。3. 鞏固;堅定,持久不變。
  • and : n. 1. 附加條件。2. 〈常 pl. 〉附加細節。
  • 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...
  • aircraft : 飛機(單復數同)
  1. Flight mechanics. concepts, quantities and symbols stability and control of aircraft

    飛行力學概念量和符號飛機穩定性和操縱性
  2. The mathematical model of new type aircraft arresting system is established in detail, and the unique solution of differential equation and the stability and the motion and control characteristics of the system are proved and analyzed

    詳細建立了新型飛機攔阻系統的數學模型,並對微分方程解的唯一性、系統的穩定性及運動特性、控制特性進行了證明、分析。
  3. This platform is used for testing the performance of su - 27 aircraft and 31e - mk optoelectronic collimation integrated system. it uses all - digital servo control system to enhance the performance of the simulation platform in order to get higher precision and better stability

    其用於在內場檢測蘇二七飛機31e - mk光電瞄準綜合系統的工作性能,在本模擬狀態中採用全數字伺服控制系統,使模擬轉臺控制精度更高,穩定性更好。
  4. Secondly, the article studies the stability, control performance and reconfiguration ability of the aircraft in theory when the differential tail is used

    其次,本文對於差動平尾所引起的飛機穩定性、控制性能的變化及重構能力進行了理論研究。
  5. Flight dynamics - concepts, quantities and symbols - part 4 : concepts, quantities and symbols used in the study of aircraft stability and control

    飛行動力學.概念量及符號.第4部分:研究飛行器穩定性及操縱性用的概念量和符號
  6. Form the practical engineering point of view, the longitudinal natural stability of anti - submarine helicopter is analyzed, the stabilized loop of the pitch angle is systematically studied. this paper is mainly on the design and simulation of the stabilized loop of pitch angle with classic control method and fuzzy control method and many useful results are achieved. the main work of this paper can briefly described as follows : after the mathematical models of aircraft was build with relevant date, the stabilized loop of pitch angel was designed and simulated

    本文從工程應用的角度出發,分析了國產直九c反潛直升機的縱向自然穩定性,分別應用古典控制和模糊控制的方法,系統地研究了國產直九c直升機的縱向姿態角穩定迴路、速度迴路、高度迴路、自動過渡等,對縱向姿態角穩定、速度、高度、自動過渡迴路進行了控制律的設計與模擬,取得了良好的控制效果。
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