跟蹤制導雷達 的英文怎麼說

中文拼音 [gēnzōngzhìdǎoléi]
跟蹤制導雷達 英文
track and guidance radar
  • : Ⅰ名詞(腳的後部或鞋襪 的後部) heel Ⅱ動詞1 (在後面緊接著行動) follow 2 (指嫁給某人) be marrie...
  • : 名詞(腳印; 蹤跡) footprint; track; trace; trail
  • : Ⅰ動詞1 (製造) make; manufacture 2 (擬訂; 規定) draw up; establish 3 (用強力約束; 限定; 管束...
  • : 動詞1. (引導) lead; guide 2. (傳導) transmit; conduct 3. (開導) instruct; teach; give guidance to
  • : 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...
  • 跟蹤 : follow the tracks of; tail after; following; follow up tracing; track; tracking; trail; lock on; ...
  • 雷達 : [訊] radar (縮自 radio detection and ranging)
  1. Tracking - and - guiding radar

    跟蹤制導雷達
  2. For missile, either strategical or tractical, the most important thing is to attack the target accurately. this depends upon the accurate location of the larget by the missile radar. for protecting radar antenna from external environment and for air - dynamical requirement, a radome is used to enclose the antenna. but the radome interferes in the orientation of the antenna, degradaties its perfor - mance, decreases the power reaching the target, and most importantly, it produces so called boresight error ( bse ) that is, makes the antenna shows a slightly different direction of the target from its true direction, the boresight error is define as the angle shifted, and the boresight error slope ( bses ) is defined as the ratio of angle shift to the tracing angle of the radar antenna. to predict the boresight error and boresight error slope is an unavoiding chief task in designing radome and in its operation

    在戰略和戰術彈中,一項重要的工作就是對目標的準確,這取決于對目標的準確定位。為了保護天線不受外界環境的影響,天線罩被應用進來,但天線罩在保護天線不受外界惡劣環境影響的同時對天線電磁輻射產生某些干擾,使天線的電氣性能降低,影響天線的功率傳輸,更重要的是產生瞄準誤差。它使目標的視在位置與真實位置有一個角度差,這個角度差就是天線罩的瞄準誤差。
  3. Abstract : angular glint error ( age ) is the main factor affecting angle tracking of millimeter wave ( mmw ) radar seeker so must be suppressed

    文摘:角閃爍誤差是影響毫米波引頭末階段精度的主要因素,必須對其進行抑
  4. An on - line minimum - variance estimator was developed for thrust acceleration applied to orbit transfer using discrete - time radar measurements. the mass - flow - rate of propellant was selected as a state variant, which was estimated by employing an integral state model and ekf filter. the variation equations for measurement vector to mass - flow - rate have been established to linearize the discrete - time measurement equations. the algorithm has applied successfully to maneuver process in commanding satellite into geo - stationary orbit. the results show that the algorithm developed here can monitor and determine whether engine works well or failure precisely and quickly during orbit transfer process

    飛行器軌道機動過程中,為、定位機動目標和干預機動控過程,需要統計處理離散的觀測量實時估計推進發動機的推力,進而確定飛行器的瞬時軌道參數.本文所述演算法是該工程問題的探討和解決方案.文章建立了軌道機動過程中連續變質量運動模型和離散量測模型,推進發動機的質量秒耗量作為表徵推力加速度的一個近似常量,應用擴展卡爾曼濾波對離散的測量數據進行順序統計處理給出秒耗量的最小方差估計;文章詳細地推了線性化量測模型的變分方程和觀測矩陣;模擬結果表明該演算法能快速、準確地估計推進發動機的質量秒耗量和向機動目標施加的實際推力
  5. The design of a data display system on the guidance radar monitor with 8098 single - chip computer is demonstrated

    摘要介紹了8098單片機與顯示器組成的靜默數據顯示系統的設計與實現。
  6. To solve the resource problem of anti - missile radar omnidirectional and high data rate tracking targets, missile self - position technology to improve missile position precision based on the scheme of passive bd is put forward

    摘要為了解決近程防空實現全方位、高數據率多自標、截獲彈遇到的資源緊張問題,提出了利用bd無源定位方案實現彈自定位,提高彈自定位精度的方法。
  7. Active and passive radar composite seeking ( aprcs ) technology is one of multi - mode composite seeking technologies. it is the typical application of information fusion technology in target tracking field

    主被動復合技術是一項雙模復合尋的技術,是信息融合技術在目標領域的典型應用。
  8. As active and passive radar composite seeking technology balances the tackle performance, design complexity and expenditure of a missile guided system, there will still be great potential of such technologies in current and future theater assault and defense systems

    這使該技術在當前及未來的戰場攻防體系中具有很強的應用前景。信息融合演算法設計是主被動復合技術的核心,其本質屬于多傳感器多目標融合演算法范疇。
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