雷達交接 的英文怎麼說

中文拼音 [léijiāojiē]
雷達交接 英文
radar hand off
  • : 1. (雲層放電時發出的響聲) thunder 2. (軍事上用的爆炸武器) mine 3. (姓氏) a surname
  • : Ⅰ動詞1 (暢通) extend 2 (達到) reach; attain; amount to 3 (通曉; 明白) understand thoroughly...
  • : Ⅰ動詞1 (把事物轉移給有關方面) hand over; give up; deliver 2 (到某一時辰或季節) reach (a cert...
  • : Ⅰ動詞1 (靠近;接觸) come into contact with; come close to 2 (連接; 使連接) connect; join; put ...
  • 雷達 : [訊] radar (縮自 radio detection and ranging)
  1. High precision ad chip is used for intermediate frequency data sampling and fpga of virtex - series is used for the implementation of intermediate - frequency orthogonal system, which includes the sequencing control design for mult - channel radar system with verilog, the application of ip core of digital filter and fifo, as well as the communication control module with dsp. as the master control part, the software programming for the communication between dsp and fpga is designed. the experimental result with hardware circuit shows the design is valid and practical

    採用高精度的adc晶元完成中頻采樣,通過virtex -系列fpga設計中頻正系統,主要包括通過verilog語言實現多路中頻收的時序控制,通過濾波器ip核實現濾波器的設計,以及利用c語言實現dsp的通訊控製程序設計。並給出了fpga在資源和速度上一些優化的方法,調試過程中影響中頻正收性能測試的因素。
  2. The successful launch and return of shenzhou - vi, marks that our aerospace technology has entered the era of large - scale near - space exploitation and utilization. in the near future, the technology is directly expected to serve for national economy. in order to develop the space experiment and research on its application, it is imperative to build a permanent space station., where rendezvous and docking plays an important role. meanwhile, the technology of the rendezvous lidar is pivotal for rendezvous and docking

    神六的成功發射和返回,標志著我國的航天事業進入了大規模開發和利用近地空間的新階段。為了開展空間科學試驗和應用技術研究,就必須建設永久性空間站。空間會對技術是建立空間站的關鍵技術,而空間會激光技術又是空間會中的關鍵技術。
  3. This thesis discusses the pulse doppler ( pd ) weather radar signal processing system including digital intermediate frequency ( if ) receiver, especially on the application of if sampling and digital demodulation technique in pd weather radar signal processing system, the influence of amplitude and phase unbalances of in - phase and quadrature channels on weather radar echo spectrum estimation, ground clutters elimination algorithms and a typical engineering realization scheme of pd weather radar signal processing system

    本論文研究的是採用數字中頻收技術的脈沖多普勒氣象信號處理系統,重點研究了中頻采樣及數字解調技術在脈沖多普勒氣象信號處理系統中的應用、正雙通道幅相不平衡對氣象回波譜估計的影響、地雜波濾波演算法,以及脈沖多普勒氣象信號處理系統的具體工程實現。
  4. In this paper. the question of compound guidance about mid - long range air - to - air missle to be considered. the main contributions are as follows : first, two midcourse guidance laws are given. that is optimally predictable pn micourse guidance, which is suitable for middle range missle, and singularly perturbed midcourse guidance. which is suitable for long range missle guidance ; then two terminal guidance laws are given. that is variable structure guidance, which is suitable for passive radar guidance. and optimal guidance which is suitable for active radar guidance ; and then the error sourses of hand - off are researched, the hand - off law is given at the time ; fmally, the midcourse guidance laws and terminal guidance laws are tested by simulation, and the whole trajectory simulation are given through hand - off law, and the results are satisfied

    主要工作如下:首先研究了用於中遠程空空導彈復合制導的兩種中制導律,即用於中程導彈的最優預測比例導引中制導律和用於遠程導彈的奇異攝動中制導律,它們均有很好的中制導性能,能夠滿足中末制導的班要求;著研究了兩種末制導律,即用於被動末制導的變結構制導律和用於主動導引頭的最優末制導律,均適用於復合制導末制導段;然後分析了中末制導的班誤差源,討論了用於復合制導的律;最後通過模擬,驗證了提出的中制導律和末制導律,結合提出的規律,在不同的情況下對中末制導段彈道進行了模擬驗證,結果證明文中提到的中末制導律能夠到性能指標要求。
  5. Thus the main and auxiliary polarization radars form a side lobe canceller system. based on the modeling of this system, an anti - jamming filter algorithm in the polarization - spatial domain is brought forward

    針對收全極化,在其旁邊放置全向雙極化正陣列天線與構成旁瓣對消系統,並根據系統模型提出了極化域-空域聯合濾波抗干擾演算法。
  6. In this paper, a design of pseudo - code cw rendezvous and docking ( rvd ) radar signal processor is presented

    摘要介紹了某偽碼連續波會對信號處理機設計。
  7. In chapter 2, first give the theory of phased array radar. second introduce the analog t / r module and digital t / r module. third discusses some key technology of wide band digital t / r module, including ddws technology and quadrature modulate technology. at last present a scheme of l bandwide banddigital t / r module

    第二章首先介紹了相控陣系統的組成和工作過程,其次介紹了模擬t / r組件和數字t / r組件的組成,然後介紹了寬帶數字t / r組件的關鍵技術,包括:直數字波形產生技術和正調制技術,最後提出了一種l波段寬帶數字t / r組件的框圖。
  8. The rendezvous docking is one of the key technologies of setting up space station, while the rendezvous laser radar ( rvr ) is one of the key & difficult points of rvd

    空間會對技術是建立空間站的關鍵技術之一,而空間會激光的apt技術又是空間會中的關鍵也是最困難的技術之一。
  9. Radar data processing ( rdp ) is critical technology in air traffic control ( atc ) system. rdp receive observation from sensor and processing radar data to tracking target. rdp provide position, velocity, characters and maneuver of target

    數據處理是空中通管制系統中的關鍵技術,它傳感器獲取的數據並進行相應的處理,形成表示目標運動軌跡的航跡,提供目標的位置,速度,機動情況和屬性識別,對目標進行跟蹤和監視。
  10. The tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided

    研究復合制導的戰術導彈中末制導班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例,結合導彈運動方程組和目標運動模型,計算了中末制導班的導引頭預定參數,並計算了在制導站測量誤差下的末制導導引頭預定參數的計算精度.可知,導引頭定位參數的計算誤差隨著彈目距離的近而顯著增大,得到中末制導班不能太晚的重要結論
  11. Abstract : the tactical missile seeker handover accuracy from midcourse to terminal guidance is researched. the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources. firstly, the terminal guidance seeker presetting parameters are computed, based on the equations of a surface - to - air missile movement and a target movement. then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed. it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target, which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided

    文摘:研究復合制導的戰術導彈中末制導班的導引頭預定精度問題.提出用小擾動法分析導引頭預定參數對誤差源的誤差敏感性關系.以中遠程防空導彈為例,結合導彈運動方程組和目標運動模型,計算了中末制導班的導引頭預定參數,並計算了在制導站測量誤差下的末制導導引頭預定參數的計算精度.可知,導引頭定位參數的計算誤差隨著彈目距離的近而顯著增大,得到中末制導班不能太晚的重要結論
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