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Dynamics modeling and control design method for long-term deorbiting of an electrodynamic tether system
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Jia-hui YAN1, Ti CHEN1, Hao WEN1, Cao-qun LUO1, Wen-xuan PENG2, Wei-dong YUN2
Journal of Vibration Engineering | 2024, 37(10) : 1792 - 1802
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Journal of Vibration Engineering | 2024, 37(10): 1792-1802
Dynamics modeling and control design method for long-term deorbiting of an electrodynamic tether system
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Jia-hui YAN1, Ti CHEN1, Hao WEN1, Cao-qun LUO1, Wen-xuan PENG2, Wei-dong YUN2
Affiliations
  • 1State Key Laboratory of Mechanics and Control for Aerospace Structures,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
  • 2Shanghai Institute of Aerospace System Engineering,Shanghai 201108,China
Published: 2024-10-28 doi: 10.16385/j.cnki.issn.1004-4523.2024.10.018
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This paper investigates the dynamics and control problems of the long-term deorbiting of an electrodynamic tethered satellite system. The dynamics modeling of the system is carried out based on a dumbbell model assumption. To improve the accuracy of the system model,the orbital dynamics is described using a set of modified equinoctial elements,involving the effects of Lorentz force,atmospheric drag and J2 perturbation force. Three current control strategies are proposed to regulate the electrodynamic forces for achieving a stable long-term deorbiting process,namely,the constant current input,the directionally variable current input,and the optimal control strategies. In the design of the optimal control strategy,the long-term deorbiting problem is formulated as an inverse problem of dynamics with nonlinear constraints,which is further solved via a nonlinear programming method to obtain the optimal reference trajectories. The deorbiting of the system is then achieved using the modified current control input obtained from a tracking feedback control law. Additionally,an energy-based current switch control strategy is adopted to ensure the stability of system and the efficient utilization of Lorentz force. Case studies of the system with designed physical parameters are conducted to analyze the deorbiting efficiency and to validate the effectiveness of the proposed control strategies.

tethered satellite system  /  electrodynamic  /  optimal control  /  long-term deorbiting
Jia-hui YAN, Ti CHEN, Hao WEN, Cao-qun LUO, Wen-xuan PENG, Wei-dong YUN. Dynamics modeling and control design method for long-term deorbiting of an electrodynamic tether system[J]. Journal of Vibration Engineering, 2024 , 37 (10) : 1792 -1802 . DOI: 10.16385/j.cnki.issn.1004-4523.2024.10.018
Year 2024 volume 37 Issue 10
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Article Info
doi: 10.16385/j.cnki.issn.1004-4523.2024.10.018
  • Receive Date:2024-05-19
  • Online Date:2026-02-12
  • Published:2024-10-28
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  • Received:2024-05-19
  • Revised:2024-07-15
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Affiliations
    1State Key Laboratory of Mechanics and Control for Aerospace Structures,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
    2Shanghai Institute of Aerospace System Engineering,Shanghai 201108,China
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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