A Posture Data Equivalent Alternative Method on Space Tracking Ship

摘要：

　　The difference of Inertia navigation device distribution between traditional space TT&C ship and new space TT&C ship is discussed.Since the design for Inertia navigation device distribution can affect observation mode and ship posture data usage,ship posture alternative problem is raised base on the analysis of space TT&C ships design.The problem is conversed to a universal 2 point posture alternative problem.The equivalent posture matrix at fault point is obtained,through two equivalent coordinate transformation processes.Then posture data at fault point is obtained by solving equations.At last,the alternative method is tested by using space TT&C ships flight check data.

关键词： equivalent posture matrix space TT&C ship Inertia navigation distribution fault point

作者: Xiang Jie Mao Yong-xing Zhang Yun

作者单位: China Satellite Maritime Tracking and Controlling Department,Jiangyin,China Jiangyin Polytechnics college Jiangyin,China

会议类型: 国际会议

会议名称: 2017 IEEE 3rd Information Technology and Mechatronics Engineering Conference(ITOEC2017)(2017 IEEE 第3届信息技术与机电一体化工程国际学术会议)

会议地点: 重庆

会议语种:英文

页码: 46-49

在线出版日期: 2017-10-03（万方平台首次上网日期，不代表论文的发表时间）