基于二阶全驱系统的航天器姿态避障控制
鲁明, 陈雪芹, 吴凡, 曹喜滨
Attitude maneuver control of spacecraft based on second⁃order fully actuated system under attitude constraints
Ming LU, Xueqin CHEN, Fan WU, Xibin CAO
航空学报
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2024, (1): 628958
-628958
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DOI: 10.7527/S1000-6893.2023.28958
CJA