Improved maximum likelihood method for ship parameter identification

被引:0
作者
Chen, Hongli [1 ]
Li, Qiang [1 ]
Wang, Ziyuan [2 ]
机构
[1] Harbin Engn Univ, Coll Automat, Harbin 150001, Heilongjiang, Peoples R China
[2] China Elect Technol Grp Corp, Inst 34, Hefei 230000, Anhui, Peoples R China
来源
2018 37TH CHINESE CONTROL CONFERENCE (CCC) | 2018年
关键词
Vessel; parameter identification; state estimation; Maximum likelihood; nonlinear filtering; NONLINEAR-SYSTEMS;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
An improved maximum likelihood method is proposed to estimate the state estimation problem of the unknown hydrodynamic parameters in the nonlinear state space equation of a ship. On this basis, a new nonlinear filtering algorithm, Belief Condensation Filtering, is studied. A new likelihood probability formula is derived. Further, a new calculation strategy of expectation and maximization of two stages is proposed by using Monte Carlo method and two parameter updating methods. And the theory proves that the two strategies are convergent with the updating of the parameters. The proposed algorithm is an iterative process of two stages: using the improved maximum likelihood method to identify the current time parameters, and using nonlinear filtering and identification parameters to estimate the state of the current time. The algorithm does not use all observation data to do maximum likelihood iterative computation. It only uses the observed value of current time to calculate. It is simple in calculation and can be applied to real-time online parameter identification. In view of a 3 degree of freedom nonlinear state space model for Underwater Unmanned Aerial Vehicle (AUV), the realization and results of specific identification of ship parameters are given. The simulation results show that the proposed method is effective and can be used to identify the nonlinear parameters of the ship.
引用
收藏
页码:1614 / 1621
页数:8
相关论文
共 19 条
[1]   Kalman filtering strategies utilizing the chattering effects of the smooth variable structure filter [J].
Al-Shabi, M. ;
Gadsden, S. A. ;
Habibi, S. R. .
SIGNAL PROCESSING, 2013, 93 (02) :420-431
[2]  
ANTONELLI G, 2001, CONTROL SYSTEMS TECH, V9, P756
[3]  
Chen H, 2016, 2016 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION, P2006, DOI 10.1109/ICMA.2016.7558874
[4]  
Chen T, PARTICLE FILTERS STA
[5]   Aerodynamic parameter estimation from flight data applying extended and unscented Kalman filter [J].
Chowdhary, Girish ;
Jategaonkar, Ravindra .
AEROSPACE SCIENCE AND TECHNOLOGY, 2010, 14 (02) :106-117
[6]  
Dan Yuntao, 2010, MICROCOMPUTER INFORM
[7]  
Dan Yuntao, 2010, RES PARTICLE SWARM O
[8]  
Fossen Thor I, 1994, Guidance and Control of Ocean Vehicles
[9]   Distributed consensus filtering for discrete-time nonlinear systems with non-Gaussian noise [J].
Li, Wenling ;
Jia, Yingmin .
SIGNAL PROCESSING, 2012, 92 (10) :2464-2470
[10]  
Mazuelas S, 2013, SIGNAL PROCESSING IE, P1