TY - JOUR
T1 - Uncertainty analysis of aircraft flight parameters prediction
AU - Xu, Zheping
AU - Lang, Rongling
AU - Deng, Xiaole
PY - 2012/6
Y1 - 2012/6
N2 - Flight performance parameters can be used for fault prediction and condition monitoring, which is of great importance for the improvement of flight security and reduction of aircraft maintenance costs. Since the airplane is a complicated system, its performance parameter series are always nonlinear. In addition, affected by the operating environment, driving factors and noises generated by sensors, the performance parameters are often mixed with noises, which leads to uncertainty in prediction results. In order to deal with this problem, a new method is proposed to predict flight parameters by using a nonlinear support vector machine. By adding a new restriction, the uncertainty problem is properly solved. This method can not only enhance prediction precision, but also deal with problems involving large amounts of input data by using sequential minimal optimization. The method is evaluated by simulation data and actual flight performance parameters. Test results show that this new model which takes noise into consideration exhibits an improvement in precision as compared with the original model. Thus, this new method provides better precision for flight malfunction prediction, which is of great significance in enhancing flight safety.
AB - Flight performance parameters can be used for fault prediction and condition monitoring, which is of great importance for the improvement of flight security and reduction of aircraft maintenance costs. Since the airplane is a complicated system, its performance parameter series are always nonlinear. In addition, affected by the operating environment, driving factors and noises generated by sensors, the performance parameters are often mixed with noises, which leads to uncertainty in prediction results. In order to deal with this problem, a new method is proposed to predict flight parameters by using a nonlinear support vector machine. By adding a new restriction, the uncertainty problem is properly solved. This method can not only enhance prediction precision, but also deal with problems involving large amounts of input data by using sequential minimal optimization. The method is evaluated by simulation data and actual flight performance parameters. Test results show that this new model which takes noise into consideration exhibits an improvement in precision as compared with the original model. Thus, this new method provides better precision for flight malfunction prediction, which is of great significance in enhancing flight safety.
KW - Aircraft flight parameter
KW - Exhaust gas temperature
KW - Exhaust gas temperature margin
KW - Prediction
KW - Support vector machine
KW - Uncertainty
UR - https://www.scopus.com/pages/publications/84864518536
M3 - 文章
AN - SCOPUS:84864518536
SN - 1000-6893
VL - 33
SP - 1100
EP - 1107
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 6
ER -