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	Satellite attitude controller based on a multilayer feedforward network
	Dong Zhe ; You Zheng
	2010-05-10 ; 2010-05-10
关键词	Practical Theoretical or Mathematical/ artificial satellites attitude control feedforward neural nets linear systems neurocontrollers precision engineering/ satellite attitude controller multilayer feedforward network satellite attitude dynamics attitude control precision linear control theory state response error least square criterion maneuvering angles pitching angle roll angle yaw angle/ C3360L Aerospace control C3120C Spatial variables control C1340N Neurocontrol
中文摘要	The error between satellite attitude dynamics and its linearized model can affect the attitude control precision. The model of the error was established with a multilayer feedforward network, and a new controller based on the model and linear control theory was presented. The controller realizes the decoupled control of the satellite attitude and minimizes the state response error between satellite attitude dynamics and its linearized model in the sense of the least square criterion. Simulation results show that the control precision is high when the maneuvering angles of pitching angle, roll angle and yaw angle are all 0.01 rad.
语种	英语 ; 英语
出版者	Tsinghua Univ. Press ; China
内容类型	期刊论文
源URL	[http://hdl.handle.net/123456789/24548]
专题	清华大学
推荐引用方式 GB/T 7714	Dong Zhe,You Zheng. Satellite attitude controller based on a multilayer feedforward network[J],2010, 2010.
APA	Dong Zhe,&You Zheng.(2010).Satellite attitude controller based on a multilayer feedforward network..
MLA	Dong Zhe,et al."Satellite attitude controller based on a multilayer feedforward network".(2010).

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