A Three body Close tracking Architecture for Attitude and Drag free Control of Gravity Satellite

被引：0
|
作者：
Liao H. [1 ]
Zheng D. [1 ]
Zhao Y. [2 ]
Zhu Z. [2 ]
Xie J. [2 ]
机构：
[1] School of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] Research Center, Shanghai Institute of Satellite Engineering, Shanghai
来源：
Yuhang Xuebao/Journal of Astronautics | 2022年 / 43卷 / 11期
关键词：
Attitude and drag free control; Bandwidth parameterization; Composite active disturbance rejection control; Lorentz actuator; Three body close tracking architecture;
D O I：
10.3873/j.issn.1000-1328.2022.11.007
中图分类号：
学科分类号：
摘要：
A non contact Lorentz actuator is used to replace the micropropulsion system, and a three body close tracking satellite architecture of "proof mass payload module service module" is proposed to avoid the influence of the dynamics uncertainty caused by the centroid fluctuation and the actuator in the design of traditional low low gravity tracking field measurement satellite. Secondly, the coupling attitude control and orbital control dynamics under this architecture is established, and a composite active disturbance rejection control based on bandwidth parameterization is constructed to deal with the nonlinear coupling dynamics, and to improve the attitude and drag free control performance. Finally, the extensive numerical simulation is conducted to validate the effectiveness of the proposed approach. The simulation results show that the proposed approach can be used to improve the systematic performance in the frequency domain. © 2022 China Spaceflight Society. All rights reserved.
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页码：1499 / 1510
页数：11
相关论文
共 31 条
  • [1] LUO Ziren, ZHANG Min, JIN Gang, Et al., Introduction of chinese space-borne gravitational wave detection program "Taiji"and "Taiji-1 "satellite mission [ J ], Journal of Deep Space Exploration, 7, 1, pp. 3-10, (2020)
  • [2] GOU Xingyu, WANG Lijiao, LI Mingqun, Et al., Acceleration mode drag free control of TQ 1 satellite [ J ], Journal of Astronautics, 42, 5, pp. 603-610, (2021)
  • [3] PAIL R, GOIGINGER H, SCHUH W, Et al., Combined satellite gravity field model GOCO01S derived from GOCE and GRACE, Geophysical Research Letters, 37, 20, (2010)
  • [4] ABICH K, ABRAMOVICI A, AMPARAN B, Et al., In-orbit performance of the GRACE follow-on laser ranging interferometer [J], Physical Review Letters, 123, 3, (2019)
  • [5] CANUTO E, COLANGELO L., Satellite-to-satellite attitude control of a long-distance spacecraft formation for the next generation gravity mission, European Journal of Control, 25, pp. 1-16, (2015)
  • [6] HONG S W, CONKLIN J., Finding the suitable drag-free acceleration noise level for future low-low satellite-to-satellite tracking geodesy missions, Advances in Space Research, 63, 1, pp. 32-50, (2019)
  • [7] LANGE B., The drag-free satellite, AIAA Journal, 2, 9, pp. 1590-1606, (1964)
  • [8] LANGE B., The control and use of drag-free satellites [ D ], (1964)
  • [9] FICHTER W, SCHLEICHER A, BENNANI S, Et al., Closed loop performance and limitations of the LISA pathfinder drag-free control system [ C ], AIAA Guidance, Navigation and Control Conference and Exhibit, (2007)
  • [10] CAO Xibin, SHI Li, DONG Xiaoguang, Et al., An adaptive control law for autonomous formation flight [ J ], Journal of Astronautics, 33, 4, pp. 411-418, (2012)
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