Research on Self-adaptive Guidance for Space Vehicles Inject Orbit

摘要：

We can use an self-adaptive guidance method during space vehicles inject orbit. But its Jacobian inverse matrix is often singular,to deal with this situation,the thesis designed a degree reduction self-adaptive guidance for space vehicles inject orbit. In the degree reduction self-adaptive guidance method ,the thesis take the movement of the rocket apart the movement in orbit and the movement in yaw plane which is vertical to orbit plane. The results of simulations shown;the degree reduction self-adaptive guidance would be helpful to solve the problem when the Jacobian inverse matrix is singular,and the anti-perturbation ability of the degree reduction self-adaptive guidance is improved.

关键词： Space Vehicle Self-adaptive Improve Guidance Method Inject Orbit

作者: Li Jian Liu Xinjian Hou Zhongxi

作者单位: College of Aerospace and Material Engineering,National University of Defence Technology,Changsha,China,410073

会议类型: 国际会议

会议名称: The 11th International Space Conference of Pacific-basin Societies(第11届环太平洋国际航天会议)

会议地点: 北京

会议语种:英文

页码: 218-222

在线出版日期: 2007-05-16（万方平台首次上网日期，不代表论文的发表时间）