linear maximum likelihood method 中文意思是什麼

linear maximum likelihood method 解釋
線性極大似然法
  • linear : adj. 1. 線的,直線的。2. 長度的。3. 【數學】一次的,線性的。4. 【動、植】線狀的;細長的。5. 由線條組成的,以線條為主的,強調線條的。
  • maximum : n (pl maximums ma ) 極點,最大,最高,最高額,最大值;最高點;最大限度;【數學】極大(值)(opp...
  • likelihood : n. 1. 可能(性)。2. 【數、統】似然,似真。3. 〈古語〉希望,前途。
  • method : n 1 方法,方式;順序。2 (思想、言談上的)條理,規律,秩序。3 【生物學】分類法。4 〈M 〉【戲劇】...
  1. In the sense of mean squares, maximum likelihood estimator, best linear unbiased estimator, taest linear invariant estimator, and good linear estimator are contracted. fourth, proposed and researched the reliability analysis method under the zero - failure data and doof data. based on the part beta distribution as the prior distribution of failure probability p, = p ( t < r, }, hierarchical bayesian estimate method was discussed, obtain the reliability analysis method under the zero - failure data and the doof data

    第四,提出並研究了無失效數據類型和doof數據類型下電連接器的可靠性分析方法,提出了以不完全beta分佈為一級先驗分佈,超參數為[ 0 , 1 ]上的均勻分佈作為失效概率先驗分佈的多層bayes方法,結合加權最小二乘法解決了產品在無失效數據和doof數據下的可靠性分析問題。
  2. First, being based upon kalman filter, extended kalman filter formulas was established ; second, with using extended kalman filter in non - linear dynamics system maximum likelihood identification method, the self - contained formulas of estimating parameter was established ; third, according to the air layout of the missle, the aerodynamic parameters identification calculating model was gained, with applying to the non - linear dynamics system maximum likelihood identification method ; finally, with using the calculating model, the aerodynamic parameters were gained. the results which were gained from the calulating model were almost consistent with which were gained from the wind tunnel experiment. thus, it was viable to use the method to estimate the aerodynamic parameters

    首先,以卡爾曼濾波為基礎,將其推廣于非線性動力學系統,建立了廣義卡爾曼濾波算式;其次,把廣義卡爾曼濾波算式應用於非線性動力學系統最大似然演算法和非線性動力學系統最大似然遞推演算法中,建立了各自的參數估計完備算式;再其次,以所建立的傾斜穩定導彈空間運動數學模型為基礎,根據該導彈的氣動布局,推導並建立了該導彈空間運動數學模型,將最大似然遞推演算法應用其中,建立了導彈氣動力參數辨識的數學模型;最後,利用該模型,估算出了氣動力參數,所得結果與風洞實驗數據基本吻合,從而認為採用此方法是可行的。
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