@Article{cmes.2015.108.303,
AUTHOR = {Zhimin  Chen, Yuanxin  Qu, Yuming  Bo, Yongliang  Zhang, Bo  Cong, Xinfeng Yu},
TITLE = {Pseudo-Linear Kalman Filter-based GPS Active Aircraft Tracking Algorithm},
JOURNAL = {Computer Modeling in Engineering \& Sciences},
VOLUME = {108},
YEAR = {2015},
NUMBER = {5},
PAGES = {303--313},
URL = {http://www.techscience.com/CMES/v108n5/27283},
ISSN = {1526-1506},
ABSTRACT = {For the sake of a higher accuracy of active aircraft GPS tracking, the tracking algorithm based on pseudo-linear Kalman filter is hereby proposed. This algorithm simplifies geometrical and algebraic relations to obtain a pseudo-linear model, then tracking the target by means of Kalman filter algorithm. Meanwhile, the tracking algorithm is studied to build a velocity & position tracking model and a velocity & acceleration tracking model. As shown by the experimental result, the tracking algorithm based on pseudo-linear Kalman filter can meet the requirement of active aircraft GPS tracking, but also attain a higher tracking accuracy in velocity & acceleration tracking model.},
DOI = {10.3970/cmes.2015.108.303}
}