TY - JOUR
T1 - 基于PSO-BP神经网络的广播星历轨道误差预测模型
AU - Peng, Yaqi
AU - Xu, Chengdong
AU - Niu, Fei
AU - Zheng, Xueen
AU - Wang, Yiwen
N1 - Publisher Copyright:
© 2019, Editorial Office of Systems Engineering and Electronics. All right reserved.
PY - 2019/7/1
Y1 - 2019/7/1
N2 - In the practice of satellite navigation data processing, it is found that there is uncertainty and regularity in the broadcast ephemeris orbit error. For the reason that this kind of error information cannot be represented by a definite mathematical model, an error prediction model based on the particle swarm optimization back propagation (BP) neural network is established. In this model, the particle swarm optimization (PSO) is used to globally optimize the initial weights and thresholds of the BP neural network. The satellite position and velocity, calculated by broadcast ephemeris, with time information and perturbation correction parameters, are combined together to train and test the neural network. The results show that model's fitting ability and prediction effect to the broadcast ephemeris orbit error are better. This model can be used to provide error compensation for satellite position calculation, so the accuracy of satellite orbit determination can be improved effectively and the system-level error can be reduced.
AB - In the practice of satellite navigation data processing, it is found that there is uncertainty and regularity in the broadcast ephemeris orbit error. For the reason that this kind of error information cannot be represented by a definite mathematical model, an error prediction model based on the particle swarm optimization back propagation (BP) neural network is established. In this model, the particle swarm optimization (PSO) is used to globally optimize the initial weights and thresholds of the BP neural network. The satellite position and velocity, calculated by broadcast ephemeris, with time information and perturbation correction parameters, are combined together to train and test the neural network. The results show that model's fitting ability and prediction effect to the broadcast ephemeris orbit error are better. This model can be used to provide error compensation for satellite position calculation, so the accuracy of satellite orbit determination can be improved effectively and the system-level error can be reduced.
KW - Back propagation neural network
KW - Broadcast ephemeris orbit error
KW - Particle swarm optimization (PSO)
KW - Perturbation correction parameters
UR - http://www.scopus.com/inward/record.url?scp=85073693353&partnerID=8YFLogxK
U2 - 10.3969/j.issn.1001-506X.2019.07.24
DO - 10.3969/j.issn.1001-506X.2019.07.24
M3 - 文章
AN - SCOPUS:85073693353
SN - 1001-506X
VL - 41
SP - 1617
EP - 1622
JO - Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
JF - Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
IS - 7
ER -