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中国科学院数学与系统科学研究院机构知识库
KMS Of Academy of mathematics and systems sciences, CAS
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2020 [1]
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中国科学. 数学 [1]
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动力下降制导问题的两阶段序列凸化方法
期刊论文
中国科学. 数学, 2020, 卷号: 50, 期号: 9, 页码: 1361-1374
Authors:
杨沐明
;
攸国攸
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Submit date：2021/01/14
rocket
powered descent guidance
optimal control
convexification
two-stage
火箭
动力下降制导
最优控制
凸化
两阶段
