摘要
在重量轻、功耗低和可靠性高等较高技术要求下,采用光纤陀螺与GPS组合定姿定轨技术,作为微小型航天器或舱外机动装置上高精度自主姿态确定系统,文中重点研究了光纤陀螺与GPS组合定姿在航天器定姿中的应用情况。
In order to meet the requirements of advanced technology on low weight, low consumed power and high reliability, the integrated FOG/GPS are used as a high precision attitude determination system. In this paper, the application of integrated FOG/GPS system on spacecrafts attitude control is studied.
出处
《中国惯性技术学报》
EI
CSCD
2004年第1期49-54,共6页
Journal of Chinese Inertial Technology
