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浏览/检索结果: 共6条，第1-6条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Research on the strategy method for the final translation phase of space autonomous rendezvous 会议论文 10th World Congress on Intelligent Control and Automation, WCICA 2012, Beijing, China, 2012-07-06 作者:  Li, Nan;  Liu, Zhenghua;  Li, Huifeng;  Zong, Xiaoxiao 收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06 Attitude quaternion control in the final approach phase of rendezvous and docking by sliding mode control 会议论文 10th World Congress on Intelligent Control and Automation, WCICA 2012, Beijing, China, 2012-07-06 作者:  Zong, Xiaoxiao;  Liu, Zhenghua;  Ren, Yan;  Li, Nan 收藏  |  浏览/下载：3/0  |  提交时间：2020/01/06 Design of 3-D discrete sliding mode variable structure guidance law for air missile 会议论文 10th World Congress on Intelligent Control and Automation, WCICA 2012, Beijing, China, 2012-07-06 作者:  Chang, Le;  Liu, Zhenghua;  Zong, Xiaoxiao 收藏  |  浏览/下载：3/0  |  提交时间：2020/01/06 Attitude Quaternion Control in the Final Approach Phase of Rendezvous and Docking by Sliding Mode Control 会议论文 PROCEEDINGS OF THE 10TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA 2012), 2012-01-01 作者:  Zong Xiaoxiao;  Liu Zhenghua;  Ren Yan;  Li Nan 收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06 rendezvous and docking  attitude control  attitude quaternion  sliding mode control   Design of 3-D Discrete Sliding Mode Variable Structure Guidance Law for Air Missile 会议论文 PROCEEDINGS OF THE 10TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA 2012), 2012-01-01 作者:  Chang Le;  Liu Zhenghua;  Zong Xiaoxiao 收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06 three-dimensional space  discrete sliding mode guidance law  variable structure  robustness   Research on the Strategy Method for the Final Translation Phase of Space Autonomous Rendezvous 会议论文 PROCEEDINGS OF THE 10TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA 2012), 2012-01-01 作者:  Li Nan;  Liu Zhenghua;  Li Huifeng;  Zong Xiaoxiao 收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06 terminal  autonomous rendezvous  guidance method  orbit control