Airborne navigation database(NavDB)coding directly affects the result of analysis on the instrument flight procedure by the modern aircraft flight management computer(FMC).A reasonable flight track transition mode can...Airborne navigation database(NavDB)coding directly affects the result of analysis on the instrument flight procedure by the modern aircraft flight management computer(FMC).A reasonable flight track transition mode can improve the track tracking accuracy and flight quality of the aircraft.According to the path terminator(PT)and track transition characteristics of the performance based navigation(PBN)instrument flight procedure and by use of the world geodetic system(WGS)-84 ellipsoidal coordinate system,the algorithms for“fly by”and“fly over”track transition connections are developed,together with the algorithms for coordinates of fix-to-altitude(FA)altitude termination point and heading-to-an-intercept(VI)track entry point and for track transition display of the navigation display(ND).According to the simulation carried out based on the PBN instrument approach procedure coding of a certain airport and the PBN route data at a high altitude,the algorithm results are consistent with the FMC-calculated results and the actual ND results.展开更多
针对目前Turbo码分量编码器参数识别算法容错性不好、计算量大的缺点,该文提出一种基于校验方程符合度的新算法。首先,根据码元约束长度较小的特点,构建出编码器生成多项式数据库,然后通过遍历多项式数据库,计算出每种多项式所对应的平...针对目前Turbo码分量编码器参数识别算法容错性不好、计算量大的缺点,该文提出一种基于校验方程符合度的新算法。首先,根据码元约束长度较小的特点,构建出编码器生成多项式数据库,然后通过遍历多项式数据库,计算出每种多项式所对应的平均校验方程符合度值,其最大值所对应的索引号即为多项式库中的正确多项式索引号,从而完成编码多项式的识别。该算法仅仅遍历有限的多项式数据库,其计算量较小,只与截获的数据量有关;算法采用的数据为软判决信息,故其容错性能较好。仿真结果表明:在信噪比为0 d B条件下,仅需要截获10码块,交织长度为100的码元数据量,参数的识别率就能达到90%以上。展开更多
基金supported by the National Natural Science Foundation of China(u2133209)。
文摘Airborne navigation database(NavDB)coding directly affects the result of analysis on the instrument flight procedure by the modern aircraft flight management computer(FMC).A reasonable flight track transition mode can improve the track tracking accuracy and flight quality of the aircraft.According to the path terminator(PT)and track transition characteristics of the performance based navigation(PBN)instrument flight procedure and by use of the world geodetic system(WGS)-84 ellipsoidal coordinate system,the algorithms for“fly by”and“fly over”track transition connections are developed,together with the algorithms for coordinates of fix-to-altitude(FA)altitude termination point and heading-to-an-intercept(VI)track entry point and for track transition display of the navigation display(ND).According to the simulation carried out based on the PBN instrument approach procedure coding of a certain airport and the PBN route data at a high altitude,the algorithm results are consistent with the FMC-calculated results and the actual ND results.
文摘针对目前Turbo码分量编码器参数识别算法容错性不好、计算量大的缺点,该文提出一种基于校验方程符合度的新算法。首先,根据码元约束长度较小的特点,构建出编码器生成多项式数据库,然后通过遍历多项式数据库,计算出每种多项式所对应的平均校验方程符合度值,其最大值所对应的索引号即为多项式库中的正确多项式索引号,从而完成编码多项式的识别。该算法仅仅遍历有限的多项式数据库,其计算量较小,只与截获的数据量有关;算法采用的数据为软判决信息,故其容错性能较好。仿真结果表明:在信噪比为0 d B条件下,仅需要截获10码块,交织长度为100的码元数据量,参数的识别率就能达到90%以上。
