flight characteristics 中文意思是什麼
flight characteristics
解釋
飛行特性- flight : n 1 飛行，飛翔；（鷹對獵物的）追趕。2 （候鳥等的）遷徙；飛行的一群。3 （光陰）飛逝。4 （思想等的...
- characteristics : 產品性能描述
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In - flight refuelling equipment. dimensional and functional characteristics of connections
空中加油設備.接頭的尺寸和功能特性 -
Thus the flight dynamic characteristics and control features in the conversion mode are the key technologies in the whole tilt rotor design
過渡模式飛機的氣動布局改變主要體現在縱向平面內，所以本文主要研究過渡模式下飛機縱向通道的動力學特性和控制系統設計。 -
A mathematical model reflecting the tilt rotor unsteady and nonlinear aerodynamic characteristics in the longitudinal channel is presented in the paper. in the full flight envelope, the rotor thrust continues tilting and the aerodynamic forces of each component change as a function of airspeed and nacelle angle
在整個飛行包線內，旋翼的推力矢量方向不斷變化，飛機各部件的氣動力隨發動機短艙傾角和空速的變化而變化，因而飛機的飛行動力學有很強的非定常、非線性特性。 -
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。 -
Influence of spraying distance on flight characteristics and deformation of particle
噴塗距離對粒子飛行特徵及變形程度的影響 -
Analyzing to a stand off missile ' s flight characteristics, the as missile trajectory simulation is completed
在分析了典型防區外導彈飛行特點的基礎上，進行空地導彈彈道模擬。 -
The composite grips extend bearing life, while working with the innovative two - stage dampening to give the n9 incredible flight characteristics
綜合槍柄軸承延長壽命，同時與創意兩階段調高給n9不可思議的飛行特性 -
Not only does the photo show a flying saucer, but the flight characteristics described by the witness defy conventional aerial motion because the object was moving rapidly, stopped, hovered, and then sped off
不僅圖片表現出飛碟，但飛行特性描述的證人藐視常規空中議案，是因為物體移動快，停，盤旋，然後迅速趕過 -
In order to study the flight characteristics and control rules in taking off and landing period better to promote flight safety of uav in this stage, we started the study of take off and landing simulation system research of uav based on a certain type of uav
為更好地研究無人機在起飛、著陸階段的飛行特性，控制規律，以保證無人機在這一階段的飛行安全，我們以某型無人機為對象進行無人機的起飛、著陸模擬系統研究。 -
The flight characteristics of high altitude long endurance uav are analyzed, several typical kinds of aeronautical weather are ingathered, and the vertical distributing model of large scale windfield is established, traditional numerical simulation methods of atmosphere environment are summarized. 2
分析了高空長航時無人機的飛行特點，統計了幾種的典型航空氣象特徵，並提出大尺度風場的垂直分層型，最後總結了大氣風場的常用數值模擬方法； 2 -
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。 -
According to the characteristics of the load on the canopy, the method for measuring the load on the canopy with a pressure sensor is presented, and then the flight measurement of the load spectrum of the canopy is realized for the first time
根據實測活動艙蓋載荷曲線特點，提出了任務類型劃分方法，建立了活動艙蓋載荷譜數據統計方法和載荷譜編制方法，並依此編制出k8飛機活動艙蓋載荷譜。 -
The flight ' s atmospheric dynamic characteristics is considered, the aircraft is modeled as a combination of objects. most compositions, such as scene system, flight system, flight ' s sound and control surface are all simulated
）等建模軟體建立了相應的三維表現模型；模擬了飛機的主要系統：飛行系統、視景系統、儀表系統和音響系統。 -
It supports the aircraft during parking and endures the loads during ground maneuvers. most of the vertical and horizontal kinetic energy are absorbed and dissipated by landing gear. it plays an extreme important role in preventing the airframe from vibration and excessive impact forces, improving passenger comfortable characteristics and increasing aircraft flight safety
飛機起落架作為飛機結構的一個重要部件，承受著飛機與地面接觸時產生的靜、動載荷，吸收和消耗飛機在著陸撞擊、跑道滑行等地面運動時所產生的能量，在減緩飛機發生振動，降低飛機地面載荷，提高乘員舒適性，保障飛機飛行安全等方面發揮著極其重要的作用。 -
Based on the basic principle of matrix analysis and the guiding policy for air flight route planning, and in connection with the characteristics of the domestic air service as well as their market environment, according to the article, the traditional method of matrix analysis is creatively applied to airlines ' flight route planning to provide air companies with a kind of effective, strategic analysing tool in their efforts to correctly do air route planning amid the fierce competition of the market
摘要基於矩陣分析的原理和航線規劃的原則，結合中國航空公司的特點和市場環境，將傳統的矩陣分析方法應用於航空公司航線規劃中，為航空公司在激烈的市場競爭中進行正確的航線規劃提供了一種有效的戰略分析工具。 -
Paragliding equipment - paragliders - requirements and test methods for classifying flight safety characteristics
滑翔降落傘設備.滑翔傘.飛行安全特徵分類的要求和試驗方法 -
Paragliding equipment - paragliders - part 2 : requirements and test methods for classifying flight safety characteristics
滑翔降落傘設備.滑翔傘.第2部分:飛行安全特徵分類的要求和試驗方法 -
Firstly, the study about flight icing is reviewed at the beginning. the condition of icing accretion, the style of icing accretion, the parameters of icing accretion in flight, and the influence of icing accretion on the aerodynamic characteristics of an airplane are analyzed
首先，回顧了國內外在飛機結冰方面的研究情況，對飛機在飛行中的結冰條件、結冰類型、結冰參數以及結冰對氣動特性的影響進行了分析討論。 -
Analysis methods and its development about effect of ice accretion on aircraft flight dynamics characteristics
結冰對飛機動力學特性影響的分析方法及其進展 -
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。
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