Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations

Jian-cheng FANG; Ke SUN

doi:10.1631/jzus.C1100350

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Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations

计算机与自动化 | Updated：2022-12-09

- Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations
- Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations
- 信息与电子工程前沿（英文） 2012年13卷第5期页码：328-338
- Affiliations：
  
  1.National Key Laboratory of Inertial Technology, Beihang University, Beijing 100191, China
  2.Novel Inertial Instrument & Navigation System Technology Key Laboratory of Fundamental Science for National Defense, Beihang University, Beijing 100191, China
- Author bio：
  
  Ke SUN, kekeesun81@aspe.buaa.edu.cn
- Funds：
  
  Project supported by the National High-Tech R & D Program (863) of China (No. 2008AA12A216) and the National Basic Research Program (973) of China (No. 2009CB72400101C)
- DOI：10.1631/jzus.C1100350
  中图分类号： V529.1;TP13
- 收稿：2011-11-28，
  
  修回：2012-;4-;9，
  
  纸质出版：2012-05
- Accepted：
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Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations[J]. 信息与电子工程前沿（英文）, 2012,13(5):328-338.

Jian-cheng FANG, Ke SUN. Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(5): 328-338.
Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations[J]. 信息与电子工程前沿（英文）, 2012,13(5):328-338. DOI： 10.1631/jzus.C1100350.

Jian-cheng FANG, Ke SUN. Composite disturbance attenuation based saturated control for maintenance of low Earth orbit (LEO) formations[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(5): 328-338. DOI： 10.1631/jzus.C1100350.

摘要

Abstract

Maintenance of high performance formation control is important for low Earth orbit (LEO) formation missions of small spacecraft. In this paper

a model of nonlinear relative motion dynamics is built

and then nonlinear and important perturbations affecting the formation configuration

such as

and atmospheric drag

are analyzed as disturbances. Global navigation satellite system based relative positioning with nonlinear filtering is adopted to provide state information associated with the perturbations. By combining disturbance observer based control with

∞

state feedback

a composite disturbance attenuation controller is proposed for maintenance of continuous and accurate formation. With consideration of precise control relying on micro thrusters

a composite disturbance attenuation based saturated controller is designed and its stability is proved. Finally

through numerical simulations

we demonstrate that control accuracy is improved after effectively avoiding perturbations and that stabilization can be satisfied using this method.

关键词

Keywords

references

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