機動目標 的英文怎麼說

中文拼音 [dòngbiāo]
機動目標 英文
maneuvering target
  • : machineengine
  • : Ⅰ名詞1 (眼睛) eye 2 (大項中再分的小項) item 3 [生物學] (把同一綱的生物按彼此相似的特徵分為幾...
  • : Ⅰ名詞1 [書面語] (樹梢) treetop; the tip of a tree2 (枝節或表面) symptom; outside appearance; ...
  • 機動 : 1 (利用機器開動的) motor driven; motorized2 (權宜; 靈活) flexible; expedient; mobile; manoeuv...
  • 目標 : 1. (對象) target; objective 2. (目的) goal; aim; destination
  1. Study of algorithm for maneuvering target state estimator

    機動目標狀態估計器演算法研究
  2. In order to solve the problems of space group formation and event detection in battlefield, a novel group formation algorithm for maneuvering target was proposed

    摘要為了解決空間合群和戰場中的事件檢測問題,提出了一種新的機動目標的空間群生成演算法。
  3. By analyzing the movement of maneuvering targets, the changing rule of angle vectors is summarized in the time field, and then some new vectors are introduced to modify the former residual error

    通過對機動目標分析,總結出角度向量在時間域中的變化規律,通過引入新的計算向量,對原演算法殘差計算進行了修正。
  4. Backed up by the soplat theory based on particle kinematics, the second chapter of this paper presents with analysis and simulation of several single observer passive measurement models, which uses such relative movement parameters as bearings changing rates and centrifugal acceleration information on the basis of bearings measurements. in the third chapter, the observability of location respectively using bearings and its changing rates information and centrifugal acceleration information is analyzed, and its observable condition is got. the fourth chapter puts forward the modified covariance extended kalman filtering ( mvekf ) against the defect of traditional extended kalman filtering ( ekf ), whose performance is simultaneously compared in the chapter with the performance of ususal tracking algorithm such as ekf, mgekf, iekf by computer simulation

    在近年來提出的基於質點運學原理的單站無源定位理論基礎上,本文第二章提出了幾種在角度測量的基礎上增加角度變化率及相對運的離心加速度等運學參數的單站無源測量模型,並對它們進行了分析和模擬;第三章分別對利用角度及其變化率信息定位和利用離心加速度信息定位的可觀測性進行分析並得到了相應的可觀測條件;第四章針對傳統擴展卡爾曼( ekf )方法的缺點,提出了一種修正協方差的擴展卡爾曼濾波( mvefk )方法,並將其和ekf 、 mgekf 、 iekf等常用的單站無源定位濾波方法進行了性能模擬比較;第五章通過引入雷達機動目標跟蹤方法和模型,提出了利用角度及其變化率對輻射源跟蹤的多級噪聲自適應方法和imm方法;第六章主要對角度變化率和離心加速度參數的獲取技術進行了研究,提出了幾種高精度測量脈沖序列多普勒頻率變化率的方法。
  5. They are lock - on, fire - and - forget ( in arma ) missiles that are perfect for knocking out tanks and other priority vehicle targets

    它們是用雷達自跟蹤,發射后不管(武裝突襲中)的用打擊坦克和其它機動目標的首先武器。
  6. This design method overcomes the traditional autopilot ' s disadvantage that should shift the autopilot ' s gain according to flight phase ; it also can make the btt missile fly stably along the whole trajectory, and can intercept a maneuvering target accurately

    該設計方法克服了傳統自駕駛儀在控制導彈飛行中需逐段切換增益的不足,能控制btt導彈在大空域內沿全彈道穩定飛行,並能精確攔截機動目標
  7. Simulation studies show that the proposed law in this paper has better guidance accuracy and better dynamic property during pursuit - control processing and it is superior to proportional navigation

    模擬結果表明,給出的導引律在攻擊機動目標時制導精度高、脫靶量小,導引控制過程具有良好的態性,性能明顯優于傳統的比例導引律。
  8. Design of evaluation decision support system on hitting effect of maneuver targets on sea

    海上機動目標打擊效果評估決策支持系統設計
  9. An algorithm of tracking a maneuvering target based on ir sensor and radar in dense environment

    復雜環境下紅外機動目標跟蹤演算法研究
  10. Tracking algorithm of infrared maneuvering target in dense clutter

    演算法的雜波環境下機動目標跟蹤研究
  11. Maneuvering multitarget tracking algorithm based on fuzzy information

    基於模糊信息下的一種多機動目標跟蹤演算法
  12. A novel algorithm for maneuvering target tracking

    一類新型機動目標跟蹤演算法
  13. In this dissertation, the data process ( dp ) subsystem and radar control program ( rcp ) subsystem of gbr simulation system have been studied and discussed. the main work and innovation of this dissertation is as follows : ( 1 ) track filter, the basic element of track system, has been researched. we analyze the advantage and disadvantage of common target kinematic model such as constant velocity model, constant acceleration model, noval statistic model

    本文是基於某gbr模擬系統的合作項中,本人負責的數據處理子系統和雷達控製程序子系統的研究和開發的結果,主要進行的工作和創新有: ( 1 )基於跟蹤系統最基本的要素-跟蹤濾波,分析了當前常用的微分多項式模型, cv與ca (常速與常加速)模型,時間相關模型, noval統計模型,以及機動目標「當前」統計模型等模型的優缺點和雷達的觀測誤差。
  14. In order to study on fire efficiency for the rocket - assisted torpedo, this paper has gone deeply into every stages of air trajectory and underwater trajectory, and established the fire efficiency model of the rocket - assisted torpedo with the monte - carlo

    摘要為解決火箭助飛魚雷的作戰使用問題,需要確定它對隨機動目標的射擊效率,通過對該雷空中及水下彈道的各階段深入細致的分析研究,建立了火箭助飛魚雷射擊效率模擬模型。
  15. Target state estimater ( tse ) is an important and indispensable part of integrated flight and fire control system ( iffcs ). this article takes the ground mobile object as the study model. it established the system state equation and observation equation from the perspective of promoting system accuracy, simplifying the calculation and facilitating the engineering realization, the tse was set up by using the kalman filtering calculation method in the wake of linearizing the observation equation to make it adapt the precondition

    狀態估計器是綜合飛行/火力控制系統中的一個重要組成環節,本文以地面機動目標為模型,從提高估計精度、簡化計算以及便於工程實現為出發點,建立的狀態方程及觀測方程,並對其進行線性化,利用自適應卡爾曼濾波演算法構造狀態估計器。
  16. All of the algorithms above can be combined as a maneuvering target tracking system on the self - organizing sensor networks

    上述各部分演算法可以結合為自組織傳感器網路下的機動目標跟蹤系統。
  17. Maneuver target tracking based on importance resampling particle filter

    基於重要性重采樣粒子濾波器的機動目標跟蹤方法
  18. Thirdly, the theory of single radar multi - target tracking ( kalman filter algorithm, dynamic target model, track ' s origination and expiration, the form of tracking - door and association algorithm ) is dicussed, which is turned the basis of multi - radar centralized - system ' s tracking algorithm

    對單雷達的多跟蹤理論(卡爾曼濾波、機動目標模型、航跡起始與終結、跟蹤門的形成和互聯演算法)進行了系統的研究,以此作為點跡處理之後集中式多雷達系統跟蹤技術的基礎。
  19. Due to energy spread of return target signals between doppler cells, both false alarms and missed alarms increased

    機動目標回波能量在多普勒單元間的擴展還會導致弱的漏檢和虛警率的提高。
  20. 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

    飛行器軌道過程中,為跟蹤、定位機動目標和干預控制過程,需要統計處理離散的雷達觀測量實時估計推進發的推力,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.文章建立了軌道過程中連續變質量運模型和離散雷達量測模型,推進發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雷達測量數據進行順序統計處理給出秒耗量的最小方差估計;文章詳細地推導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、準確地估計推進發的質量秒耗量和向機動目標施加的實際推力
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