Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach
This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization...
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| Published in | Journal of systems science and complexity Vol. 35; no. 2; pp. 623 - 640 |
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| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
Beijing
Academy of Mathematics and Systems Science, Chinese Academy of Sciences
01.04.2022
Springer Nature B.V |
| Subjects | |
| Online Access | Get full text |
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| Abstract | This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization control of combined spacecraft. The stability of the system is proved by introducing Lyapunov function. Numerical simulation of the combined spacecraft and physical experiment based on the combined spacecraft simulator (CSS) are completed. Both simulation and experiment results demonstrate the effectiveness and practicability of the optimal controller of fully-actuated system. |
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| AbstractList | This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization control of combined spacecraft. The stability of the system is proved by introducing Lyapunov function. Numerical simulation of the combined spacecraft and physical experiment based on the combined spacecraft simulator (CSS) are completed. Both simulation and experiment results demonstrate the effectiveness and practicability of the optimal controller of fully-actuated system. |
| Author | Duan, Guangquan Liu, Guo-Ping |
| Author_xml | – sequence: 1 givenname: Guangquan surname: Duan fullname: Duan, Guangquan email: 19B904022@stu.hit.edu.cn organization: Center for Control Theory and Guidance Technology, Harbin Institute of Technology – sequence: 2 givenname: Guo-Ping surname: Liu fullname: Liu, Guo-Ping email: liugp@sustech.edu.cn organization: Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Department of Electronic and Electrical Engineering, Southern University of Science and Technology |
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| CitedBy_id | crossref_primary_10_1016_j_isatra_2024_09_010 crossref_primary_10_1007_s11424_022_2000_0 crossref_primary_10_1061_JAEEEZ_ASENG_5294 crossref_primary_10_1080_00207721_2024_2315223 crossref_primary_10_1109_TSMC_2023_3346469 crossref_primary_10_1007_s11424_024_3414_7 crossref_primary_10_1109_TCST_2023_3286044 crossref_primary_10_1080_00207721_2024_2317349 crossref_primary_10_1109_TCYB_2024_3457584 crossref_primary_10_1109_TIE_2023_3290250 crossref_primary_10_1007_s11432_022_3817_5 crossref_primary_10_1109_TIE_2023_3260355 crossref_primary_10_1016_j_jfranklin_2023_04_003 crossref_primary_10_1007_s11424_024_3539_8 crossref_primary_10_1016_j_jfranklin_2023_05_010 crossref_primary_10_1109_TSMC_2024_3519436 crossref_primary_10_1007_s00034_024_02623_3 crossref_primary_10_1016_j_jfranklin_2025_107613 crossref_primary_10_1109_TCYB_2024_3482320 crossref_primary_10_1016_j_isatra_2023_03_041 |
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| Snippet | This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is... |
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| SubjectTerms | Attitudes Complex Systems Control Controllers Liapunov functions Mathematics Mathematics and Statistics Mathematics of Computing Operations Research/Decision Theory Optimal control Orbital stability Simulation Spacecraft Spacecraft stability Statistics Systems Theory |
| Title | Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach |
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