| A Novel Sliding-mode Guidance Law Based on Lie-group Method |
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| 作者姓名： | 韩大鹏 孙未蒙 刘昆 |
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| 作者单位： | HAN Da-peng,LIU Kun(College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073 Hunan, China);SUN Wei-meng(College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073 Hunan, China;Ordnance Revamping Factory of Unit No.92854, Zhanjiang 524005 Guangdong, China;College of Mechatronic Engineering and Automation, Nation) |
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| 摘 要： |
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A Novel Sliding-mode Guidance Law Based on Lie-group Method |
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| HAN Da-peng,SUN Wei-meng,LIU Kun.A Novel Sliding-mode Guidance Law Based on Lie-group Method[J].Journal of China Ordnance,2010,6(1):25-34. |
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| Authors: | HAN Da-peng SUN Wei-meng LIU Kun |
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| Affiliation: | [1]College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073 Hunan, China [2]Ordnance Revamping Factory of Unit No. 92854, Zhanjiang 524005 Guangdong, China [3]College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073 Hunan, China |
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| Abstract: | |
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| Keywords: | control and navigation technology of aircraft multi-constraint guidance Lie group control sliding-mode control |
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