TY - JOUR
T1 - Self-calibration Kalman filter method
AU - Fu, Hui Min
AU - Wu, Yun Zhang
AU - Lou, Tai Shan
AU - Xiao, Qiang
PY - 2014/6
Y1 - 2014/6
N2 - A self-calibration Kalman filter(SKF)method, whose model and recursive algorithm were established, was presented. In most practical cases, such as deep space exploration and engine fault diagnosis, because of the effect of unknown inputs, such as gust, fault and unknown system error, the well-known Kalman filter will lead to greater filtering error in recursive process. To solve this problem, the proposed SKF, which is applied to estimate and compensate the unknown inputs, efficiently reduces the effect of the unknown inputs and enhances filtering accuracy. For some spacecraft navigation simulation, the mean and variance of estimated state errors by SKF decreased by at least 400% and 300%, respectively. The SKF method can be effective to improve the performance of filter, simple to calculate and easy to apply in engineering.
AB - A self-calibration Kalman filter(SKF)method, whose model and recursive algorithm were established, was presented. In most practical cases, such as deep space exploration and engine fault diagnosis, because of the effect of unknown inputs, such as gust, fault and unknown system error, the well-known Kalman filter will lead to greater filtering error in recursive process. To solve this problem, the proposed SKF, which is applied to estimate and compensate the unknown inputs, efficiently reduces the effect of the unknown inputs and enhances filtering accuracy. For some spacecraft navigation simulation, the mean and variance of estimated state errors by SKF decreased by at least 400% and 300%, respectively. The SKF method can be effective to improve the performance of filter, simple to calculate and easy to apply in engineering.
KW - Deep space exploration
KW - Fault diagnosis
KW - Filtering accuracy
KW - Self-calibration Kalman filter(SKF)
KW - Unknown input
UR - https://www.scopus.com/pages/publications/84903900496
U2 - 10.13224/j.cnki.jasp.2014.06.015
DO - 10.13224/j.cnki.jasp.2014.06.015
M3 - 文章
AN - SCOPUS:84903900496
SN - 1000-8055
VL - 29
SP - 1363
EP - 1368
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 6
ER -