maximum likelihood identification造句
例句與造句
- in this paper which was in the background of some model antitank missle, adopting maximum likelihood identification method estimated the aerodynamic parameters of the missle, with using flight datas
本文以某型反坦克導(dǎo)彈為背景,利用導(dǎo)彈飛行試驗數(shù)據(jù),應(yīng)用最大似然遞推算法估算了該導(dǎo)彈的氣動力參數(shù)。 - 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(chǔ),將其推廣于非線性動力學(xué)系統(tǒng),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(yīng)用于非線性動力學(xué)系統(tǒng)最大似然算法和非線性動力學(xué)系統(tǒng)最大似然遞推算法中,建立了各自的參數(shù)估計完備算式;再其次,以所建立的傾斜穩(wěn)定導(dǎo)彈空間運動數(shù)學(xué)模型為基礎(chǔ),根據(jù)該導(dǎo)彈的氣動布局,推導(dǎo)并建立了該導(dǎo)彈空間運動數(shù)學(xué)模型,將最大似然遞推算法應(yīng)用其中,建立了導(dǎo)彈氣動力參數(shù)辨識的數(shù)學(xué)模型;最后,利用該模型,估算出了氣動力參數(shù),所得結(jié)果與風(fēng)洞實驗數(shù)據(jù)基本吻合,從而認(rèn)為采用此方法是可行的。 - 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(chǔ),將其推廣于非線性動力學(xué)系統(tǒng),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(yīng)用于非線性動力學(xué)系統(tǒng)最大似然算法和非線性動力學(xué)系統(tǒng)最大似然遞推算法中,建立了各自的參數(shù)估計完備算式;再其次,以所建立的傾斜穩(wěn)定導(dǎo)彈空間運動數(shù)學(xué)模型為基礎(chǔ),根據(jù)該導(dǎo)彈的氣動布局,推導(dǎo)并建立了該導(dǎo)彈空間運動數(shù)學(xué)模型,將最大似然遞推算法應(yīng)用其中,建立了導(dǎo)彈氣動力參數(shù)辨識的數(shù)學(xué)模型;最后,利用該模型,估算出了氣動力參數(shù),所得結(jié)果與風(fēng)洞實驗數(shù)據(jù)基本吻合,從而認(rèn)為采用此方法是可行的。 - It's difficult to find maximum likelihood identification in a sentence. 用maximum likelihood identification造句挺難的