编队航天器协同绕飞非合作目标的全驱预设性能控制
收稿日期: 2023-04-21
修回日期: 2023-05-15
录用日期: 2023-06-28
网络出版日期: 2023-07-07
基金资助
国家自然科学基金(62103446);湖南省自然科学基金(2022JJ20081);飞行动力学技术重点实验室基金(KJW6142210210306);中南大学创新驱动计划项目(2023CXQD066)
Fully-actuated prescribed performance control of spacecraft formation for flying cooperatively around non-cooperative target
Received date: 2023-04-21
Revised date: 2023-05-15
Accepted date: 2023-06-28
Online published: 2023-07-07
Supported by
National Natural Science Foundation of China(62103446);Fund of Hunan Provincial Natural Science(2022JJ20081);Funding of Science and Technology on Aerospace Flight Dynamics Laboratory(KJW6142210210306);Central South University Innovation-Driven Research Program(2023CXQD066)
殷泽阳 , 邢友朋 , 韩飞 , 魏才盛 , 廖宇新 . 编队航天器协同绕飞非合作目标的全驱预设性能控制[J]. 航空学报, 2024 , 45(1) : 628904 -628904 . DOI: 10.7527/S1000-6893.2024.28904
To address the cooperative control problem of using spacecraft formation for approaching and flying around the non-cooperative target， a distributed prescribed performance control method based on the fully-actuated system theory is proposed in consideration of external interference and unexpected orbital maneuvers. First， a relative dynamic model for the service spacecraft formation and the non-cooperative target is established based on the line-of-sight coordinate system， and the fully-actuated control law is constructed to reduce the complexity of controller design. Furthermore， a distributed agreed-time prescribed performance controller is designed using the topology theory to ensure the control performance of the spacecraft formation around the target. In addition， an extended state observer is employed to observe and compensate for the uncertainties and disturbances in the system， thereby improving the control precision and robustness in spacecraft formation flying around the target. Finally， the effectiveness of the designed control method is verified by two sets of flying around simulations.
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