Regid-Flxible Coupling Dynamic Modeling and Attitude Simulation of Gravity-Gradient Satellite

摘要：

Based on the model of cantilever beam, a mathematic model of a gravity-gradient satellite is constructed in this paper by using modal synthesis method. To damp and control the satellite, a magnetic coil is applied on the z axis of the body coordinate system. After some attitude simulation, we get the result which denotes that the flexibility of the gravity gradient boom will not affect the stability of the satellite.

关键词： regid-flxible coupling:cantilever beam:modal synthesis method:magnetic damping

作者: Jian-Bin Han Hai Huang Xin-Sheng Wang

作者单位: Beihang University,Beijing,China.

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 1313-1316

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）