flight load 中文意思是什麼
flight load
解釋
飛行載荷-
It is an important half hardware - in - loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight
它是地面半實物模擬系統中的一種重要專用設備，用來模擬飛行器舵機在飛行過程中所承受空氣動力力矩載荷。 -
When testing begins, the computer of the tested uav flight control system will be connected into the network as a slave. the master of the system will diagnose faults should there be any ; otherwise it will set flight parameters and load flight course data for the slave
檢測時，無人機的飛控系統計算機作為從機連入網路，如果從機的飛控系統沒有故障，主機將為從機設置飛行參數和裝定航線數據；如果有故障，則主機為從機飛控系統診斷故障。 -
During helicopter slung - load flight, the main flight quality modes include : phugoid, dutch roll, longitude and latitude slung - load oscillation. according to the ads - 33e - prf specifications, the flight stability qualities had been evaluated
直升機機外吊掛飛行過程中，體現飛行品質的運動模態主要為荷蘭滾模態、縱向浮沉振蕩模態，以及吊掛物橫向、縱向振蕩模態。 -
Load features of flight conditions on dynamic component of helicopter
直升機某動部件飛行狀態的載荷分佈特點研究 -
Main product of this company includes more than 200 varieties and more than series such as mine shaft hoisting machine series, mine hoist series, dispatch hoist series, prop - pulling hoist series, building hoist series, flight conveyor series, heavy - load gear reducer series and electric equipment
公司主要產品有：礦井提升機系列，礦用提升絞車系列，調度、回柱絞車系列，建築卷揚機系列，刮板輸送機系列，重載減速機系列，電氣控制設備等十幾個系列近200多個規格品種的產品。 -
The aircraft load calculation implies determination of the loads acting on the aircraft structure for flight maneuvers, flight in turbulence, landing and ground handling conditions
飛機的載荷計算就是確定飛機在機動飛行、突風飛行、著陸和地面操作過程中作用在飛機結構上的載荷。 -
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 research of load calculation is very important for flight safety of the civil aircraft
對於民用飛機來說，載荷計算的研究對于飛行安全有著非常重要的意義。 -
Load simulator was an important simulation system in hardware - in - loop flight simulation laboratory, which could simulate aerodynamic loads acting on flight vehicle, such as unmanned aerial vehicle, planes
負載模擬器是半實物模擬實驗室中模擬無人機等飛行器在飛行中舵面所受空氣動力載荷的重要設備。 -
The main factors which affected the flight stability quality included : forward flight speed, slung - load and helicopter mass ration, slung - load aerodynamic forces and cable length, etc. through adjusting the above structure and performance parameters, rational flight parameters can be decided, which can ensure the safe helicopter mission operations of the slung - load flight
影響飛行品質穩定性要求的主要因素為:直升機飛行速度、吊掛物/直升機質量比、吊掛物氣動特性、吊掛鋼索長度等。通過對上述結構參數、性能參數的調節，可確定合理、經濟的飛行參數，保證安全、高效的完成直升機機外吊掛飛行運輸任務。 -
Compared with non - slung - load flight, additional aerodynamic load, gravity load should be considered in the slung - load system. so the moment to the gravity center, flight mode and the natural frequency will change
直升機吊掛飛行，與直升機非吊掛飛行狀態相比，增加了新的氣動載荷、重力載荷，和因此產生的對直升機重心的力矩，其飛行運動模式、低頻振蕩固有頻率均發生改變。 -
In some military application such as aviation 、 space flight 、 missile 、 radar and so on, the 10kv isolation voltage is needed, on the basis of it, linearity, capacity of driving load capacitance and reliability are presented
同時，在航空航天、導彈、雷達等軍事應用上，對光電耦合器提出了10kv以上的隔離電壓的要求，在此基礎上，對線性度、驅動容性負載的能力以及可靠性都有很高的要求。 -
It is manned by a flight crew of two or three and a mission crew of three and can carry 4000 kg of freight or passengers in the hold, and 5000 kg of freight carried as a slung load
卡- 27裝備獨聯體海軍航空兵印度及南斯拉夫海軍。卡- 27總體布局為共軸反轉的3片槳葉，槳葉是全復合材料，可折疊，不可收放四輪式起落架。 -
In the condition of non - axisymmetrical stage separation in hypersonic flight, the problems of dynamics and kinematics of the validating vechicle and the launch vechicle are primarily analysised. it includes the movement of the center of mass and the rigid body of the vechicles, the relative movement of the different vechicles, the relative movement of the special parts of the different vechicles, the load analysis and the probable collision in the process of stage separation
研究了在高超聲速狀態下非對稱級間分離過程中，驗證飛行器與運載火箭分離時的相關運動學和動力學問題。包括:飛行體質心運動和剛體運動;不同飛行體之間的相對運動;不同飛行體上特殊部位之間的相對運動;分離過程中各相關飛行體上的載荷分析和分離過程中可能發生的碰撞問題。 -
To solve the problems caused by the varieties of the missile dynamics with the difference of flight height, velocity and attitude angle in modeling the missile, in this thesis, the theory of variable structure model reference adaptive control is used to design a pitch channel autopilot based on a longitudinal missile model, the status equation using the measurable parameters of load and angular rate is established, and the methodology to choosing the reference model is discussed also, and the performance of the controller is analyzed by means of simulation
為了解決攔截彈氣動參數隨飛行高度、速度、姿態的不同，變化范圍大，控制系統難以準確建模的困難，基於縱向平面攔截彈模型，採用模型參考變結構控制理論設計了俯仰通道姿控復合控制系統，以可測量變量過載和角速度作為狀態量建立了系統的狀態方程，討論了參考模型的選擇方法，並對系統的性能作了模擬分析。 -
Here, active means defined shifts in load take place during the flight manoeuvre in order to investigate the flying characteristics
在這里，實際模擬就是在為了研究飛行特性而進行的飛行演習中，所產生的力的變化情況。 -
The relationship between the load measured by strain method and the load calculated according to flight parameters and the wind tunnel test data has been investigated in this thesis. the result showed that the calculation load based on the flight parameters and wind tunnel test data is acceptable in subsonic speed and gets good agreement, with the load measured by strain method
本文研究了採用應變法實測載荷和根據飛行實測參數和風洞實驗數據計算載荷之間的關系，研究表明採用飛行實測參數和風洞實驗的數據計算載荷在亞音速范圍內是可行的，與採用應變法實測載荷是吻合的。 -
It also can cooperate with acars system to provide data for oil consume analyse and technique evaluate, etc. this article discuss the working principle and realization of airplane flight safety real time monitor system, the core technology of real time database ( tplus tree index ) in detail, etc. while decoding module is one of the key modules, this article also introduces a high efficiency and easy extending qar data decoding arithmetic, the design and apply to background database, and the relative data load method in this module
本文對飛機飛行安全狀態實時監控系統的工作原理、實時數據庫的關鍵技術（ tplus樹索引）和飛機飛行實時監控系統的實現等，進行了詳細的探討。由於譯碼模塊是該系統的核心模塊之一，同時本文也介紹了一種高效的可擴展的qar數據譯碼平臺的設計和實現，以及后臺數據庫的設計和應用。同時本文也介紹了高效的數據導入的方法以及數據庫的性能優化。 -
The slung - load flight is one of the main uses of helicopter in both military and civilization domain
直升機吊掛飛行機外運輸，是其主要用途之一，在軍事、民用領域中的應用均十分廣泛。 -
This paper specially studied the math modeling of the slung - load in flight, and the math model of the whole helicopter / slung - load system as well
本文著重研究了吊掛物在飛行過程中的運動數學模型，及直升機/吊掛物整個系統的數學模型的建立。
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