TY - JOUR
T1 - An IMM-UKF with adaptive factor for GPS/BD-2 satellite navigation system
AU - Dong, Ning
AU - Xu, Yu Jiao
AU - Liu, Xiang Dong
N1 - Publisher Copyright:
©, 2015, China Spaceflight Society. All right reserved.
PY - 2015/6/30
Y1 - 2015/6/30
N2 - In this paper, a novel adaptive filter algorithm is proposed to improve position accuracy of the GPS/BeiDou-2(BD-2) integrated satellite navigation system for a maneuver vehicle in the presence of model and noise statistics uncertainty. Firstly, a new adaptive UKF is proposed to solve the problem of noise uncertainty by use of an adaptive factor obtained from the smoothing filter based on the residual error treated as the uncertainty of process noise. This adaptive method significantly reduces the effect of noise uncertainty on filtering performance. Secondly, in our method, a set M of models is taken into consideration and a 'soft switching' among the model set based on model probability is carried out by using interactive multiple model (IMM) algorithm, by which the position error caused by the model uncertainty can be reduced. The simulation results verify the effectiveness of the proposed method, and show preferable position accuracy for the complex maneuver vehicle.
AB - In this paper, a novel adaptive filter algorithm is proposed to improve position accuracy of the GPS/BeiDou-2(BD-2) integrated satellite navigation system for a maneuver vehicle in the presence of model and noise statistics uncertainty. Firstly, a new adaptive UKF is proposed to solve the problem of noise uncertainty by use of an adaptive factor obtained from the smoothing filter based on the residual error treated as the uncertainty of process noise. This adaptive method significantly reduces the effect of noise uncertainty on filtering performance. Secondly, in our method, a set M of models is taken into consideration and a 'soft switching' among the model set based on model probability is carried out by using interactive multiple model (IMM) algorithm, by which the position error caused by the model uncertainty can be reduced. The simulation results verify the effectiveness of the proposed method, and show preferable position accuracy for the complex maneuver vehicle.
KW - Adaptive
KW - Interactive multiple model
KW - Model uncertainty
KW - Noise statistics uncertainty
KW - Satellite navigation system
KW - Unscented Kalman filter
UR - http://www.scopus.com/inward/record.url?scp=84939779107&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2015.06.008
DO - 10.3873/j.issn.1000-1328.2015.06.008
M3 - Article
AN - SCOPUS:84939779107
SN - 1000-1328
VL - 36
SP - 676
EP - 683
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 6
ER -