空間模擬器 的英文怎麼說

中文拼音 [kōngjiān]
空間模擬器 英文
space simulator
  • : 空Ⅰ形容詞(不包含什麼; 裏面沒有東西或沒有內容; 不切實際的) empty; hollow; void Ⅱ名詞1 (天空) s...
  • : 間Ⅰ名詞1 (中間) between; among 2 (一定的空間或時間里) with a definite time or space 3 (一間...
  • : 模名詞1. (模子) mould; pattern; matrix 2. (姓氏) a surname
  • : 動詞1. (設計; 起草) draw up; draft 2. (打算; 想要) intend; plan 3. (模仿) imitate
  • : 名詞1. (器具) implement; utensil; ware 2. (器官) organ 3. (度量; 才能) capacity; talent 4. (姓氏) a surname
  • 空間 : space; enclosure; room; blank; interspace
  • 模擬器 : emulator
  • 模擬 : imitate; simulate; analog; analogy; imitation; simulation模擬艙 boilerplate; 模擬電路 [電學] circ...
  1. Docking mechanism test - bed is mainly used to simulate dynamics process of two aerocraft ’ s docking on the ground, validate rationality of the mechanism ’ s design and estimate stability of the docking process

    對接機構綜合試驗臺主要用於地面兩飛行對接的動力學過程,對機構設計的合理性、對接過程中的穩定性進行驗證和評估。
  2. Problem formulation, modeling and simulation of the spacecraft attitude and trajectory control. 2

    飛行姿態和軌跡控制問題的數學分析、建以及
  3. Theory analysis and experimental simulations of pursuit - evasion problem with maneuvering target in sight coordinate system are performed using the two methods

    並應用這兩種方法針對視線坐標系的兩飛行在目標機動下的追逃進行了理論推導和實驗
  4. Solar array simulator is programmed in labview to simulate the running condition of satellite ( such as sun angle, shadow time, orbit and so on ). electronic load is programmed in labview to simulate the running condition of satellite load. by data collecting and processing, satellite power engineers can monitor and evaluate working condition of satellite power system

    該測試評估系統應用labview軟體對太陽能電池陣列進行編程,太陽能電池在各種狀態下(軌道、光照角、進出陰影等)的情況;對電子負載進行編程,衛星負載的各種變化(平均負載、短期負載和脈沖負載)情況,信號採集和數據處理單元在測試評估系統運行過程中記錄電源系統各組成部分的工作參數,據此對衛星電源系統進行測試和評估。
  5. The results suggested that there lies certain regularity in the pattern of ci and the regularity depends on definite magnitude of coriolis stimulation ; the duration and the intensity of ci are positive related to the magnitude of coriolis stimulation ; the parameters of eng accompanying ci ca n ' t be used as the objective indication of ci

    不同軸向的線加速度對科里臭利錯覺的彤響本實驗在gl 2000高級定向上,分別對x軸向線加速度為0 27gx與0gx時、 y軸向線加速度為0 27gy與0gv時等量的科里奧利加速度刺激n
  6. The parallel robot has become a hot spot for a long time because of its simple structure, high stiffness, high precision, and low movement inertia. it especially adapted to the task, which required high precision, heavy load and limited space

    並聯機人具有結構簡單、剛度好、定位精度高、動態響應快等優良特性,特別適用於高精度、大載荷且工作較小的場合,在裝配生產線、高精密機床、飛行、衛星天線換向裝置等等很多方面都有著巨大的應用價值。
  7. In the air combat simulation, since the system runs in the way of time frame cycle, the flying locus of the weapon, such as missile, changes as a dispersing function, and its movement is much faster than the target ( moving or static ) comparatively, so some errors emerge when the collision test is calculated between the weapon and the target

    摘要中,由於系統採用時幀周期方法調控系統的解算,致使導彈等武的飛行彈道呈離散函數變化,而導彈等武的飛行相對于靶標(運動或靜止)是一個快速運動,這樣,武與靶標的碰撞解算就會引出很多誤差問題。
  8. The circui t construct ion and the relevan t schemes of the realization of the circuit are also provided, simultaneously, the source of errors and the compensation methods are discussed. all of analysises, calculation results and simulations demonstrate that the methods presented in the paper are feasible, the algorithm is effective, the realization of circuit is simple, the procedures of the design are standard, the circuit is easy to be fabricated on a monolithic, and the system can be used for processing middle - high frequence signal and be applied in low - voltage, low - power and at high speed

    在此基礎上,本文首次提出了一種基於狀態對數域濾波的一維連續小波變換實現方法、結構以及相關塊電路實現的策略,並對該方法的誤差來源與補償措施進行了討論。論文中的理論分析與計算以及結果表明,用對數域狀態濾波實現一維連續小波變換的方法可行,演算法簡單、有效,電路實現簡單,設汁過程規整,易於單片集成,適合處理中、高頻信號並運用於低電壓、低功耗、高速的場合。
  9. A rule - based structure of internal model control ( imc ) system is given, and a rule - based imc controller is built up. 5 approach for rough set based fdd is proposed, and its applicability and computational complexity is discussed

    以一個具有非線性特性的自來水加藥混凝沉澱系統為背景進行了研究,結果表明了基於粗糙集決策規則的粗糙狀態型和粗糙控制在非線性過程建與控制中的有效性。
  10. The ordovician carbonate reservoir in tahe oilfield is characterized by deep buried depth, multiple storage spaces, complex reservoir type, which lead to difficult reservoir simulation and performance prediction for the existing simulators are hard to simulate the dual porosity reservoirs

    摘要塔河油田奧陶系碳酸鹽巖油藏埋藏深,儲集多樣,儲集類型復雜,油藏和動態預測難度大,其原因主要是現有的油藏數值很難裂縫溶洞型雙重介質系統。
  11. First, it ’ s necessary to analyze the position inverse solution and positional solution. because of the nonuniqueness in the positional solution, it ’ s not easy to test the performance of the coordinated control system. so the model of nn was built to convert the vector of the length of 6 jars into the vector of the position of the motion deck

    針對運動平臺位置姿態正解的解析解非唯一性,本文建立神經網路轉換型將運動的桿長向量轉換為位置向量,結合現有實驗條件,本文訓練了針對縱向的轉換型,能夠快速、準確地完成桿長向量到位置向量的轉換。
  12. The simulation system of rendezvous and docking is the simulation equipment stimulating the aircraft ’ s movements of rendezvous and docking

    交會對接運動用以飛行的交會對接過程的設備。
  13. Based on the monte - carlo simulation, optimization of shielding layer material and their thicknesses were obtained for implementing partial shielding of semiconductor devices in space vehicles

    針對我國飛行中對半導體件較常用的局部屏蔽加固的方法,在m - c計算機的基礎上對屏蔽層材料及其厚度進行了優化設計。
  14. It has conducted an analysis of the virtual aircraft instrument system, finds out the characteristics of the system in flight simulator, and makes clear the data relationship between the virtual aircraft instrument system and other subsystems in flight simulator, including the function request as well as performance request for the system. with professional software vaps design the appearance of virtual aircraft instrument uses atn ( augment transition network model ) to develop the

    通過對整個虛儀表系統的需求分析,找到作為飛行儀表系統的自身特點,明確虛儀表系統和整個飛行及其它子系統之的數據關系,結合航儀表系統的實際應用確定虛儀表系統的功能要求和性能要求,確定虛儀表系統開發的整體方案和流程,最終開發整個飛行儀表系統。
  15. Standard practice for ionization gage application to space simulators

    用於空間模擬器的電離壓力計的標準實施規程
  16. This thesis studies the spacecraft control using nonlinear model predictive control and computer simulations are applied in it. the main results fall into two main areas. 1

    本文運用非線性型預測控制理論對飛行位置和姿態的控制進行了系統的分析、研究和計算機,在以下兩個方面取得顯著成效: 1
  17. This thesis presents the feasibility of nonlinear model predictive control implemented in spacecraft control and the optimality of increasing the control precision and decreasing the fuels expenditure. and the discussions are then focused on the simulation of spacecraft control using function - space model predictive control algorithm as mentioned below : 1

    本文的主要研究工作是探討非線性型預測控制( nmpc )應用於飛行自適應控制的可行性及對提高控制精度和減少燃料使用方面的優越性,同時利用函數型預測控制演算法( f - mpc )對飛行的位置和姿態控制進行,具體內容如下:一
  18. Namespace, and the application is deployed to a smart device or the pocket pc emulator, visual studio automatically checks to see whether the device has the microsoft. net compact framework and sql server mobile client components installed

    當您生成引用system . data . sqlserverce命名的託管應用程序並將該應用程序部署到智能設備或pocket pc時, visual studio會自動檢查設備上是否已安裝了microsoft . net compact framework和sql server mobile客戶端組件。
  19. ( 6 ) the spatial filter is introduced to avoid the damage from the hot - image. it is indicated by the numerical results that this work is valuable

    ( 6 )引入了濾波抑制熱像效應對光學元件造成的破壞,從數值來看,這種方法是行之有效的。
  20. The emulator runs in a memory address space separate from the other host applications and with the same privilege level as user space application, so any crash on the guest system won t affect the host

    在與其他宿主應用程序隔離開來的內存地址中運行,與用戶應用程序具有相同的特權,所以客戶系統的任何破壞都不會影響宿主。
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