CAJ | 학술논문

考虑到ADS-B监视系统数据存在各种误差以及低空航空器飞行特点，提出一种基于ADS-B数据的跟踪监视新方法。采用可设置判断门限实现飞行多模态间切换，在平稳航段发挥卡尔曼算法的优势，在机动航段保持RMIMM平滑稳定性能。该算法综合性能超越传统基于卡尔曼滤波的监视算法，有效克服卡尔曼滤波对高频部分反应迟钝的不足，又保留低频部分的良好跟踪特性。建立在多模态切换的基础上，实现不同模式的快速预测，为航迹预测提供基础。
고필도ADS-B감시계통수거존재각충오차이급저공항공기비행특점，제출일충기우ADS-B수거적근종감시신방법。채용가설치판단문한실현비행다모태간절환，재평은항단발휘잡이만산법적우세，재궤동항단보지RMIMM평활은정성능。해산법종합성능초월전통기우잡이만려파적감시산법，유효극복잡이만려파대고빈부분반응지둔적불족，우보류저빈부분적량호근종특성。건립재다모태절환적기출상，실현불동모식적쾌속예측，위항적예측제공기출。
Considering the various errors existed in the data from ADS-B surveillance system and the flight characteristics of low-altitude aircraft,a new algorithm for track monitoring based on ADS-B was proposed . The decision threshold was set up to achieve multi-mode switching for aircraft .The advantage of Kalman algorithm was exploited in the steady phase and the smooth and stable performance of RMIMM was used in the maneuvering phase .Comprehensive performance of the algorithm is superior to that of the conventional monitoring algorithm based on Kalman filtering .The shortcoming that the response of Kalman filter is inadequate when processing the high frequency signal is overcome while the good tracking performance of it when processing the low frequency signal is kept .Besides,the multi-mode switching based on different modes is achieved,and the future mode can be predicted rapidly .