guidance error 中文意思是什麼
guidance error
解釋
制導誤差-
The simulation of the terminal guidance procedure is carried out, and the results verified the conclusion that the interceptor can hit the target directly. at last, the effect of flight path angle error on interception performance is analyzed in detail
在此基礎上進行了動能攔截器攔截過程模擬，驗證了動能攔截器能夠直接碰撞命中彈道導彈的結論，並詳細分析了在不同相對距離的初始條件下，航向誤差對攔截性能的影響。 -
Taking intercontinental ballistic missiles as objects under research, and based on the analysis of the influence of accelerometer measurement error and gyroscope excursion error on the apparent acceleration, the error transfer model of the inertial system in a midcourse guidance segment for velocity and location is given, and the pure inertial navigation guidance error is computed with the given imu error coefficient deviations
摘要針對洲際彈道導彈，在分析加速度計測量誤差和陀螺漂移誤差對導彈視加速度影響的基礎上，給出了中制導段慣性系統對速度和位置的誤差傳遞模型，對給定的慣組誤差系數偏差進行了純慣性導航制導誤差計算。 -
Sensitivity of guidance error of tv - guided missile based on orthogonal experiments
基於正交試驗的電視制導空地導彈制導誤差靈敏度分析 -
The miss distance caused by guidance method error and the effects of perturbation are compensated in this initial guidance law
該初制導方法能補償制導方法誤差和軌道攝動對攔截脫靶量的影響。 -
Effect of the guidance error on destruction probability of anti - ship missile
反艦導彈制導誤差對摧毀概率的影響 -
( 3 ) on the basis of kalman filer algorithm and on the premise of two assumptions, namely, state estimation error of each sensor is dependent or independent, kalman filter weight fusion algorithm and modified track - to - track fusion algorithm are proposed, then improved algorithm is applied to the simulation of line - guidance and terminal - self guidance of torpedo
（ 3 ）基於卡爾曼濾波演算法，在各傳感器估計誤差相互獨立和不獨立兩種假設的前提下，給出了卡爾曼濾波加權融合演算法，在此基礎上，提出了修正的track - to - track航跡融合演算法，並將改進后的演算法應用於魚雷線導加末自導系統的模擬研究。 -
We discussed the laser - guided bomb ' s guidance law and attacking property, analyzed the influence of the three kinds of jamming on laser - guided bomb ' s attack effect, and then established the mathematic models of attacking error of laser - guided bomb under the three kinds of jamming
主要討論了激光制導炸彈的制導規律及其攻擊特性，分析了3種光電干擾方式對激光制導炸彈的攻擊效果的影響，給出了3種光電干擾情況下激光制導炸彈攻擊偏差的數學模型。 -
As far as the system observation for accuracy evaluation of carrier rocket is concerned, there may exist different types of observed data and priors. heterogeneous information means that the different information describing the different characteristics of the same object. since all of the information is relevant to the same object, the fusion is possible. it is a key problem that how to fuse the heterogeneous information to obtain the better evaluation result. therefore, the different heterogeneous information and data is thoroughly studied, moreover, the mathematical description for information fusion of different parameter priors and data is constructed in this paper. based on their relationship between different parameters, indirect prior and observation data is transformed into prior in impact point observation space, which is fused with original prior by weight determined by maximum entropy rule to obtain the mixed posterior distribution. therefore, the test results can be given by combining posterior distribution and impact error observed data. then its application on evaluating guidance systematic error is elaborated as it applies trajectory tracking data, test value of coefficients of guidance instrumentation systematic error, impact point observation data and prior. especially, the advantage of this method lies in its application in case that guidance instrumentation systematic error may not be computed precisely. finally a detailed example on evaluation of carrier rocket is given to verify the theory
為充分利用運載火箭觀測中的不同觀測空間和過程的信息來進行精度評估，針對該背景建立了異質先驗融合的數學描述.研究了飛行試驗中不同觀測空間和過程的異質先驗信息和數據，基於不同觀測過程的解析關系，將間接過程的先驗和觀測數據算出的后驗分佈轉換成落點觀測空間上的先驗，與原落點的先驗進行了最大熵加權融合，得到混合后驗分佈，從而結合落點觀測數據給出評定結果.在無法解算出精確的制導工具誤差系數的情況下，這種方法充分利用了彈道跟蹤數據、工具誤差系數的地面測試先驗值、落點先驗及落點數據，穩健性更好，準確性更高 -
A kinematics model for 3d guidance problems is derived, a new kind of nonlinear variable structure adaptive guidance law is brought up by researching the variable structural strength item, and another fuzzy variable structure guidance law with self - adapt region is realized to enhance robustness of target acceleration estimate error of guidance law
本文建立了三維空間追逃問題的數學模型;通過對變結構控制中其變結構強度項的研究，提出一種新型變結構自適應制導律;並且考慮到對變結構強度項進行模糊化，實現一種論域自調整的模糊變結構制導律，以增強制導律對目標加速度估計誤差的魯棒性。 -
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交班要求；接著研究了兩種末制導律，即用於被動雷達末制導的變結構制導律和用於主動雷達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交班誤差源，討論了用於復合制導的交接律；最後通過模擬，驗證了提出的中制導律和末制導律，結合提出的交接規律，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達到性能指標要求。 -
The effective disturbance of laser to imagining track system is validated by two experiments. one is laser irradiates ccd detectors and the other is laser disturbs ccd imaging track evaluation system. the energy of laser disturbing ir imagining guided system effectively is estimated. the guidance error sources are analyzed and the hitting probabilities are calculated before the disturbance and after it by utilizing the formula about single missile shot percentage
首先通過激光輻照面陣ccd探測器和激光干擾ccd成像跟蹤系統的兩個實驗，證明激光對成像跟蹤系統能形成有效干擾;然後對激光有效干擾紅外成像制導系統所需的能量進行估算;分析了制導誤差的來源，根據建立的導彈命中概率計算公式，具體計算激光干擾前後導彈命中概率。 -
The results of the calculation show that navigation and guidance method is successful and satisfactory. sixth, the results error of iterative guidance is analyzed
對運載火箭的整個制導過程進行實時模擬，通過模擬計算，得出了比較理想的導航和導引計算結果。 -
Modeling and simulation of fighter guidance theory based on collision error
基於相遇誤差的飛機導引方法建模與模擬 -
The paper expounds on the theory, concept and application of reed - solomon code by the brief introduction of error controlling system and channel coding, and finally finishes the design of rs code coder and decoder under the guidance of dvb - c standards by consulting the related references
本論文通過對差錯控制系統及通道編碼的簡單介紹，進而闡述了reed ? solomon碼的原理、概念和應用，參考有關文獻，完成了在dvb - c標準下對rs碼編譯碼器的演算法的程序編制和硬體的結構設計。 -
At the same time, the research of distributed object integration model, manufacturing information conversion pattern, manufacturing information transportation pattern and the error handling mechanisms, which constitute the manufacturing information exchange pattern, is conducted from the three aspects : solved problem, fundamental support technologies and solution. secondly, on the basis of the former research and the functional and technical requirements of e - manufacturing platform, which is a kind of realization carrier of e - manufacturing, a general implementation technologies frame of manufacturing information exchange pattern which suits to the e - manufacturing platform is brought forward. on the guidance of the frame, the manufacturing information transportation
在該實現框架的指導之下，結合xml和soap標準制定了網路化製造平臺中的製造信息傳輸協議和製造信息轉換協議，並在此協議的基礎上，研究了網路化製造平臺中實現製造信息交換模式的幾個重點和難點問題，制定了其解決方案，並運用xml （ extensiblemarkuplanguage ） ， soap （ simpleobjectaccessprotocol ）實現， j2ee （ java2platform ， enterpriseedition ）等軟體技術，建立了用於實現網路化製造平臺中製造信息交換的支持系統。 -
Abstract : sins initial alignment error is one of the important error sources for tactical surface to air missile precision allocation. it is necessary and advantageous to research quickly separate technique of sins initial alignment error in outfield for improving missile guidance precision
文摘:捷聯慣性導航系統的初始對準誤差是戰術地空導彈精度分配中的主要誤差源之一，研究在外場條件下初始對準誤差的快速分離方法對于提高導彈制導精度具有積極意義。 -
What ' s going on ? - ' guidance processor error. '
怎麼回事？ -導航系統錯誤 -
- what ' s going on ? - ' guidance processor error. '
-怎麼回事？ -導航系統錯誤 -
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交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，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達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接近而顯著增大，得到中末制導交班不能太晚的重要結論 -
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交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，計算了中末制導交班的導引頭預定參數，並計算了在制導站雷達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接近而顯著增大，得到中末制導交班不能太晚的重要結論
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