DocumentCode
2626845
Title
An fuzzy IMM method for tracking micro reentering USV with TDRS
Author
Pu Huang ; Li-Qiang Hou ; Guang-Dong Liang ; Ying Gao
Author_Institution
State Key Lab. of Astronaut. Dynamics, Xi´an, China
fYear
2011
fDate
27-29 June 2011
Firstpage
2039
Lastpage
2046
Abstract
Both kinematics and measurement model help process the trajectory data and estimate aerodynamic parameters of vehicle. In this paper, three dynamics are proposed, which are aerodynamics parameter´s model, acceleration´s model and α - β - γ model. The measurement model is TDRS (Tracking and Data Relay Satellite), which produces a complicated trajectory in reentering purpose. A fuzzy IMM algorithm is proposed in this paper, which through a fuzzy inference to get the matching degree of every UKF filtering model, instead of calculating model transition probabilities in IMM. With the matched degrees, the estimation from each filtering is weighted to get maneuvering target overall estimation and its covariance. Simulation results show that the FIMM algorithm performs well in tracking re-entering vehicle and estimating the aerodynamics parameters as well.
Keywords
Kalman filters; aerodynamics; fuzzy set theory; remotely operated vehicles; satellite tracking; space vehicles; target tracking; α - β - γ model; TDRS; UKF filtering model; acceleration model; aerodynamic parameter; fuzzy IMM method; fuzzy inference; kinematics; maneuvering target; matching degree; measurement model; microreentering USV; tracking-and-data relay satellite; trajectory data; unmanned space vehicle; Aerodynamics; Atmospheric modeling; Electronic mail; Filtering; Vehicle dynamics; Vehicles; Aerodynamics; Fuzzy IMM; Reentry Vehicle; Tracking Target;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Science and Service System (CSSS), 2011 International Conference on
Conference_Location
Nanjing
Print_ISBN
978-1-4244-9762-1
Type
conf
DOI
10.1109/CSSS.2011.5975023
Filename
5975023
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