landing process 中文意思是什麼
landing process
解釋
卸貨手續-
The paper described the building process of model that can identify the shock - absorber parameter of landing gear and at the same times optimize performance of system. in this paper, there are also some debate, it include identifying parameter which can not be measured, such as the air polytropic exponent and the orifice discharge coefficient of shock - absorber
本文利用復合形優化演算法建立了起落架緩沖系統參數識別與系統優化模型，對緩沖器空氣壓縮多變指數和油孔流量系數等不可測參數的識別和著陸、滑跑載荷多目標優化問題進行了討論。 -
The naval ship, as a three - dimensional object, its complicated tossing movements are the whirligig movements circling space axis. among them, the heave oscillation of the deck is an important guidance parameter for the uav ’ s landing in the process of landing
艦艇作為三維空間物體，其顛簸運動是一個復雜的繞空間軸的旋轉運動，其中艦船甲板的升沉高度是艦載無人機著艦導引系統的一個重要參數。 -
The wrf ( v1. 2 ) system is used to simulate the landing process of winnie in 1997, and results show that the track, landing time, and landing position of winnie calculated using the common land model ( clm ) and the initial field of 0800 bst on 18th august 1997 are closer to the reality ( fig. 4. 3 ) than those in the other 7 experiments, indicating the better forecast and simulation capability of the wrf model than the others
應用wrfv1 . 2版系統對1997年登陸臺風winnie進行了數值預報模擬研究，結果表明，用通用陸面模式（ clm ）對8月18日08時初始場計算得到的winnie移動路徑、登陸時間及地點（見圖4 . 3 ）比其它七個試驗的計算結果更接近實際情況。表明wrf模式有較強的預報模擬能力。 -
Now, it is worthwhile to conduct the research on the ground load of landing gear with multi - wheels and multi - struts according to the basic theories of the mechanics, the dynamics analysis model of the full - aircraft during its landing process is established in this paper
本文首先以某多輪多支柱飛機的起落架作為研究對象，應用動力學基本原理，建立了全機的著陸動力學模型。然後，通過利用大型動力學模擬軟體adams對該飛機進行了對稱著陸模擬，並對模擬結果進行了對比分析。 -
Ideally, searchers find a high - ranking site in the search engine results and navigate quickly from the landing page through a prescribed channel, ultimately through the shopping cart and checkout process
理想的搜索者在搜索引擎中找到一個排名靠前的網址，通過快速登陸頁，在通過規定的頻道，最終通過購物車和結帳的程序完成的。 -
How to precisely simulate the landing process of an aircraft and effectively absorb aircraft landing kinetic energy to attenuate the impact loads on aircraft is a problem facing the landing gear community
如何精確模擬飛機著陸過程起落架和機身的動態響應，並據此設計減小飛機著陸過程中的沖擊載荷的方案，一直是飛機起落架設計和分析中的重要課題。 -
Moreover, this text showed a 3d emulated animation for the whole process of helicopter ' s landing with dcp
另外，本文還對直升機雙攝影測量著艦過程進行了三維動畫模擬演示。 -
Chapter 4 describes the manufacture method of emulated animation showing system of helicopter landing process, helped to understand dcp livelier
第四章描述了直升機著艦模擬動畫演示系統的製作，有助於更加形象直觀的了解dcp系統。 -
In this paper we made a systemic analysis and study of the accurate orientation technology in the process of helicopter landing - photogrammetry, made the model of using double ccd to measure the exact position of helicopter based four latent points photogrammetry, educed formula about beaconing position, analyzed the computing error, and particularly computed the information of beaconing position of the helicopter ' s landing by experiment emulation. in the result, the error between a computed value and a measurement value was less than 5 centimeters
本文對直升機著艦精確定位技術中的攝影測量演算法進行了系統分析和深入研究，在四特徵點測量演算法基礎上建立了雙ccd攝影測量直升機精確位置坐標的數學模型，進一步從各個影響演算法測距精度的方面討論了計算誤差，推導出測量信標坐標位置的計算公式，並對利用雙攝影測量演算法計算直升機著艦掛鉤位置的正確性及準確性進行了模擬實驗，得到的演算法計算值和實驗測量值之間的誤差在5cm以內。 -
From the simulation, we can get some parameter curves of landing gear. by analyzing these curves and the methods with two - masses model, the linear state equation of landing gear during landing process was established
基於參數曲線分析和二質量模型建立了起落架著陸的線性狀態方程，應用現代控制理論對方程進行分析並結合matlab軟體對其進行著陸動態模擬。 -
In this competitive market where every facet of the interview process can be imperative to landing the position you strive for, alan nierenberg provides all the answers to questions you have and even more importantly, answers to questions you hadn ' t even thought of, that could make all the difference
在這個競爭市場，而每一方面的面試過程，可一定要登陸你的立場爭取，阿蘭尼倫伯格提供所有答案的問題，你還有更重要的，回答你甚至都沒有想過，這可能所有差別。 -
The flight control system contains gps & ins, which insured auto takeoff & landing, as well as the whole flight process
飛行控制系統採用gps全球定位系統和慣性導航系統，可自動完成從起飛到著陸的整個飛行過程。 -
Landing gear is one of the important equipments in the aircraft structure, it can influence the aircraft during the process of takeoff, landing and taxiing
起落架是飛機結構中的重要裝置之一，它影響到飛機的起飛、著陸和滑跑過程。 -
This thesis deeply researches the virtual reality techniques used in the spacecraft ’ s soft landing process on asteroids
本文對深空探測器在小行星表面軟著陸過程中一些虛擬現實技術進行較為深入的研究。 -
Through analysis of aircraft landing process, the paper has developed an optimized model of runway high - speed exit
摘要通過對飛機著陸過程的分析，建立了跑道快速出口優化模型。 -
In the former study of the landing process of an aircraft, modeling and analysis methods are conventional and a little bit drop behind
以往對于飛機著陸過程起落架和機身動態響應的模擬，大多對起落架系統進行理想化的簡化假設，建模和分析手段相對較為傳統。 -
They can be concluded within four parts : spacecraft substantial modeling, 3d terrain modeling, safe landing area choice and visual demonstration of the whole landing process
主要內容包括四部分:探測器實體化建模、三維地形建模、軟著陸安全區域選取以及可視化演示。 -
Computational multibody dynamics and virtual prototyping technology are brand new modeling and analysis methods for simulating the landing process of an aircraft
而計算多體系統動力學和虛擬樣機技術的出現，使得對于飛機著陸過程起落架和機身動態響應的模擬更逼近於現實。 -
Finally, the perturbation of 10 parameters and the air disturbances including horizontal wind, vertical wind and gust are considered in the landing process. the simulation results show that the designed landing system possesses not only satisfactory performances but also strong robustness
本文的最後一部分對飛機自動著陸過程中存在的風干擾作了研究，建立了垂直風、水平風的數學模型，並在風的干擾下對飛機著陸過程作了閉環模擬。 -
In this paper, dynamic analysis for landing gear landing is conducted for a large transportation aircraft, and dynamic equation of landing gear during landing process was established. the mathematical model and dynamic simulation of landing gear was established in the software adams
本文以某大型運輸機起落架為研究對象，建立了起落架著陸動力學方程，應用adams軟體對該起落架進行建模和被動控制下的著陸動態模擬，得到了相關的參數曲線。
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