DocumentCode
1794958
Title
Cooperative interception guidance for multiple vehicles: A receding horizon optimization approach
Author
Baoqing Yang ; Liu, Hugh H. T. ; Yu Yao
Author_Institution
Control & Simulation Center, Harbin Inst. of Technol., Harbin, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
827
Lastpage
831
Abstract
In the traditional terminal guidance, the state estimator and guidance law are design independently by assuming the validity of the separation principle and the certainty equivalence principle, which are only valid for linear systems with Gaussian noise. This paper considers the nonlinear terminal guidance system for a target interception problem by multiple vehicles. Firstly, the probability density function of target position at the intercept time instant is predicted based on estimates of the current state considering special environment and possible complex maneuver of the target; Secondly, the cost function related to probability density function of target position is determined, and the multi-vehicle against one target cooperative guidance method is proposed based on receding horizon optimization. Finally, simulation results show the validity of the proposed cooperative guidance approach.
Keywords
Gaussian noise; control system synthesis; missile guidance; optimisation; state estimation; Gaussian noise; certainty equivalence principle; cooperative interception guidance; cost function; guidance law design; nonlinear terminal guidance system; probability density function; receding horizon optimization; receding horizon optimization approach; separation principle; state estimator design; Acceleration; Cost function; Equations; Noise measurement; Probability density function; Simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007317
Filename
7007317
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