TY - JOUR
T1 - Real-time total system error estimation
T2 - Modeling and application in required navigation performance
AU - Li, Fu
AU - Jun, Zhang
AU - Rui, Li
N1 - Publisher Copyright:
© 2014 Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA. Open access under CC BY-NC-ND license.
PY - 2014
Y1 - 2014
N2 - In required navigation performance (RNP), total system error (TSE) is estimated to provide a timely warning in the presence of an excessive error. In this paper, by analyzing the underlying formation mechanism, the TSE estimation is modeled as the estimation fusion of a fixed bias and a Gaussian random variable. To address the challenge of high computational load induced by the accurate numerical method, two efficient methods are proposed for real-time application, which are called the circle tangent ellipse method (CTEM) and the line tangent ellipse method (LTEM), respectively. Compared with the accurate numerical method and the traditional scalar quantity summation method (SQSM), the computational load and accuracy of these four methods are extensively analyzed. The theoretical and experimental results both show that the computing time of the LTEM is approximately equal to that of the SQSM, while it is only about 1/30 and 1/6 of that of the numerical method and the CTEM. Moreover, the estimation result of the LTEM is parallel with that of the numerical method, but is more accurate than those of the SQSM and the CTEM. It is illustrated that the LTEM is quite appropriate for real-time TSE estimation in RNP application.
AB - In required navigation performance (RNP), total system error (TSE) is estimated to provide a timely warning in the presence of an excessive error. In this paper, by analyzing the underlying formation mechanism, the TSE estimation is modeled as the estimation fusion of a fixed bias and a Gaussian random variable. To address the challenge of high computational load induced by the accurate numerical method, two efficient methods are proposed for real-time application, which are called the circle tangent ellipse method (CTEM) and the line tangent ellipse method (LTEM), respectively. Compared with the accurate numerical method and the traditional scalar quantity summation method (SQSM), the computational load and accuracy of these four methods are extensively analyzed. The theoretical and experimental results both show that the computing time of the LTEM is approximately equal to that of the SQSM, while it is only about 1/30 and 1/6 of that of the numerical method and the CTEM. Moreover, the estimation result of the LTEM is parallel with that of the numerical method, but is more accurate than those of the SQSM and the CTEM. It is illustrated that the LTEM is quite appropriate for real-time TSE estimation in RNP application.
KW - Aviation
KW - Estimation
KW - Navigation
KW - Required navigation performance
KW - Total system error
UR - http://www.scopus.com/inward/record.url?scp=84927666947&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2014.10.021
DO - 10.1016/j.cja.2014.10.021
M3 - Article
AN - SCOPUS:84927666947
SN - 1000-9361
VL - 27
SP - 1544
EP - 1553
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 6
ER -