flight measurement 中文意思是什麼

flight measurement 解釋
飛行測量
  • 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...
  • measurement : n. 1. 測量，計量，量度。2. 份量，尺寸，大小，寬度，厚度，深度（等）。3. 測量法。 measurement goods （按體積、容積計算的）體積貨物。
  1. Uav ( unmanned aerial vehicle ) plays a more and more important role in national defense and civil life. so making researches on the uav flight controller design and the measurement and control techniques of uav is of theory, engineering and economical value

    無人機在軍民兩用領域發揮著越來越重要的作用，進行民用無人機飛行控制器設計及檢測與控制技術研究，具有理論意義、工程意義和經濟意義。
  2. Finally, according to the requirement that the transparent data must be exchanged interactively on space - flight and aerial distributed experiment and measurement system, the method that the distributed experiment and measurement system with the middle component of virtual shared memory is introduced, and its software wraps based on fast ethernet, rpc and broadcasting data are developed. according to the character of multi - task and high real - time in ivems, the technique of management, fault tolerance and the synchrony of multi - line are discussed detailedly

    在此基礎上針對航天、航空產品的分散式試驗與測試系統對透明數據交互的需求，採用虛擬共享內存中件構造分散式試驗與測試系統的方法，參與設計了虛擬共享內存中件，並獨立完成了基於快速以太網、 rpc和udp廣播數據的虛擬共享內存中件的通訊技術設計與實現。
  3. Firstly, the mathematical method, wavelet transform of random error processing and kalman filtering algorithm of system error estimation, is designated ; the process of development of wavelet transform and its present research is recommended ; and, the definition and development situation of real - time data processing and post - flight data processing of trajectory measurement data is summarized briefly

    首先指出了應用的數學方法，即處理隨機誤差的小波變換方法和估計系統誤差的kalman濾波演算法;介紹了小波變換方法的發展過程和國內外的研究現狀;綜述了彈道測量數據的實時數據處理和事後數據處理的概念和發展狀況。
  4. Dynamic models and measurement models of real - time data processing and post - flight data processing are given respectively. based on kalman filtering, two improved kalman filtering algorithms are obtained, which correspond to different demand of real - time data processing and post - flight data processing

    分別給出了在實時數據處理和事後數據處理中動力學模型和測量模型，根據kalman濾波思想，針對實時處理和事後處理的不同要求，得出對應的兩個改進的kalman濾波演算法。
  5. Brzozowski t m, maczynska m, zawada m, et al. time - of - flight measurement of the temperature of cold atoms for short trap - probe beam distances [ j ]. j opt b, 2002, 4 : 62

    耿濤，閆樹斌，王彥華，等.用短程飛行時間吸收譜對銫磁光阱中冷原子溫度的測量[ j ] .物理學報， 2005 ， 54 : 5104
  6. This paper adopts the traditional flight measurement - strain gauge method to figure out the problem, this is a big attempt. the result illustrates that strain gauge can be used in the dynamic measurement of recoil, and the method is effective

    本文採用飛行測量的傳統方法? ?應變電測來解決該問題，是一次大膽的嘗試，結果表明應變電測方法應用於後座力動態測量是可行的，結果是可信的。
  7. 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。
  8. Virtual instruments technology was applied to build the measurement and control system and develop the software for the experiment, which improve the efficiency of the study. finally the velocity control experiment of sapc at several flight states was accomplished which has a good effect. the study has certain significances on developing electronic - electric cpcs

    構建基於虛擬儀器技術的測控平臺，採用labview軟體開發測控軟體，利用實驗室的現有條件，結合某型電子/氣動式壓調器的實驗，完成了飛機在各種飛行狀態下所需的大氣壓力模擬艙內的壓力控制，取得了較好的效果。
  9. Optoelectronic measurement of distance using time - of - flight principle - part 1 : incoherent time - of - flight principle

    使用渡越時間法則的光電測距.第1部分:不相干的渡越時
  10. Abstract : in this paper, a new method for dynamic measurement of engineexhaust using tofms ( time - of - flight mass spectrometer ) is presented, and a high - speed data acquisition system is designed

    文摘:本文介紹了利用飛行時間質譜儀（ tofms ）對發動機發動過程中的排氣成分進行動態檢測的方法以及為此開發的高速數據採集系統。
  11. It is a novel way ( problem ) to measurement dynamically the recoil in the flight

    在飛行狀態下進行後座力動態測量是一種新的測試課題。
  12. Based on this, also described is the measurement method and request of the main antenna parameters, and carrying on the tests of antenna model, real antenna test and the flight - test, and studying and analyzing the data of all tests in the end

    在此基礎上，還闡述了天線主要參數測試方法和相關要求，並進行了隱蔽式天線縮比模型的地面測試試驗，全尺寸天線地面試驗及飛行試驗，最後對試驗數據進行了研究和分析。
  13. Design and realization of the acoustic waves flight time measurement system based on cross - correlation method

    基於互相關技術的聲波飛行時間測量系統的設計與實現
  14. In the flight experiment of aircraft, the mass data acquisition, storage and transfer is always one important part of system, especially for the measurement of parameters such as temperature and pressure of cockpit. in order to meet these needs, we design this simultaneous data acquisition system with multi - channel and large - capacity, which is based on single chip microprocessor and usb interface. it overcomes some shortcomings of traditional devices such as : big size, short work time, small memory capacity etc. it also has many advantages of high speed, low power dissipation, ease - of - use, ease to expand port, supporting plug - play, low - cost etc, so it will be used very widely

    在飛機的飛行試驗中，海量數據的採集、存儲和傳輸一直是系統非常重要的一部分，尤其是對飛行員駕駛艙環境控制系統的溫度、壓力等參數的測量來說更是如此。本文根據課題實際需要，研製的基於單片機和usb介面的多通道、大容量、便攜式數據採集系統，克服了現有設備體積大、工作時間短、存儲容量小等缺點。同時，本系統還具有功耗低、速度快、使用方便靈活、易於擴展、支持即插即用、成本低廉等一系列優點，具有廣泛的應用前景。
  15. Based on gyro - free inertial navigation theory while revolve about mems accelerometer and dsp, this dissertation mainly focuses on the research of gyro - free inertial measurement unit for shell flight path measurement - the first step for guidance

    本文以無陀螺慣性導航理論為基礎，以微機械加速度傳感器、高性能dsp處理器為核心，研製應用於某型炮彈的無陀螺慣性測量系統，該系統將用於炮彈飛行軌跡的測量，是實現炮彈制導的第一步。
  16. The author first explains that large - scale measurement device is one of the most basic measuring methods of obtaining external trajectory data and flight status. lt is pointed out that the accurateness of the main - item axis system deviation correction ( including vertical, level and collimating axis deviation ) of large - scale measurement device error is of critical importance to the precison of measuring device ' s surveying angles. to improve its precison, the influence of axis system deviation on surveying angles must be corrected

    首先說明了在現代航天靶場中，大型測量設備是獲取外彈道數據和飛行狀態的最基本的測量手段之一，指出大型測量設備測量系統誤差的主項軸系偏差（包括垂直軸偏差、水平軸偏差和照準軸偏差）改正的精確與否直接關繫到測量設備的測角精度，因此要提高測量設備的測角精度，必須對軸系偏差對測量角的影響進行改正。
  17. Acoustics - measurement of sound pressure levels in the interior of aircraft during flight iso 5129 : 2001

    聲學.飛行中飛機內聲壓級的測量
  18. According to the requirement on the testing of recoil caused by weapon launching during helicopter flighting, this paper puts forward the dynamic measurement method based on the practical situation, and resolves the problem of recoil ’ s measurement of weapon launching during helicopter ’ s flight

    本文根據直升機飛行中武器發射后坐力測量的需要，從實際情況出發，提出並設計了相應的動態測試方案，解決了在飛行狀態下武器發射後座力的測量問題。
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