复杂约束下的挠性航天器姿态参考管理控制
Explicit reference governor-based constrained flexible spacecraft attitude control
摘要
关键词
挠性航天器/姿态控制/复杂约束/模态观测器/显式参考管理Key words
flexible spacecraft/attitude control/complex constraints/modal observer/explicit reference governor引用本文复制引用
党庆庆,刘贞报,李文博,桂海潮,刘萍..复杂约束下的挠性航天器姿态参考管理控制[J].控制理论与应用,2023,40(10):1813-1820,8.基金项目
国家自然科学基金项目(11972056),国家自然科学基金优秀青年项目(62022013),广东省基础与应用基础研究基金项目(2019A1515111070),深圳市自然科学基金项目(GXWD20201231165807008,20200830220334001),科技部国家重点研发计划项目(2020YFC2200801,2020YFC2200502),航天科技集团行业特色科研项目(6230109004),陕西省自然科学基金青年项目(2023-JC-QN-0003),中央高校基本科研业务费专项资金项目(23GH020210)资助.Supported by the National Natural Science Foundation of China(11972056),the National Natural Science Funds for Excellent Young Scholars of China(62022013),the Guangdong Basic and Applied Basic Research Foundation(2019A1515111070),the Shenzhen Science and Technology Program(GXWD20201231165807008,20200830220334001),the National Key R&D Program of China(2020YFC2200801,2020YFC 2200502),the Industry specific Program of China Aerospace Science and Technology Corporation(6230109004),the Natural Science Foundation of Shaanxi Province(2023-JC-QN-0003)and the Fundamental Research Funds for the Central Universities(23GH020210). （11972056）
