original description
2.The specimen used as the basis of the original published description of a taxonomic group and later designated as the type specimen.
5.For this reason you should always bring your medicine in the original container on which is usually found the description of the dosis administration.
6.Controposed to single description coding(SDC),multiple description coding(MDC) for image is source coding in which several bit streams(descriptions) of original image are produced such that acceptable quality of the reconstructed image can be obtained from each description.
7.In this paper description is made of 12VE230ZC type diesel engine,whose rated power has been increased from 1618 kW of the original design to 2206kW,and speci- fic fuel consumption reduced from 252g/(kW·h)to 238g/(kW·h),with its speed and dimensions remaining unchanged.
8.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.
