Predictive control for satellite formation keeping

被引：0

作者：

He Donglei Cao Xibin Research Center of Satellite Technology Harbin Institute of Technology Harbin P R China ^{[150080
]}

机构：

来源：

Journal of Systems Engineering and Electronics | 2008年 / 01期

关键词：

predictive control; satellites formation; low-thrust technology; Lyapunov theorem;

D O I：

暂无

中图分类号：

V448 [制导与控制];

学科分类号：

081105 ;

摘要：

Based on a Hill equation and a nonlinear equation describing the desired and real dynamics of relative motion separately, a predictive controller is brought forward, which makes the real state track the desired ones to keep satellite formation. The stability and robustness of the controller are analyzed. Finally, comparing the simulation results of the proposed controller with that of the traditional, proportional-differential controller shows that the former one is capable of keeping the satellite formation more favorably, considering the disturbances such as the J2 perturbations.

引用

页码：161 / 166

页数：6

共 5 条

[1]

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[2]

Spacecraft formation flying: dynamics and control. Kapila V,Sparks A G. Journal of Guidance, Controlan Dynamics . 2000

[3]

Advanced guidanced algorithms for spacecraft formation keeping. Michael T,Jonathan P H. . 2002

[4]

Analysis of low thrust orbit transfers using thelagrange planetry equations. David E G. IEPC-97–160 . 1997

[5]

Nonlinear Tracking Control for SatelliteFormations. His-Han Yeh. Journal of Guidance, Control and Dynamics . 2002

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