| 微小卫星编队飞行轨道动力学及相对位置保持控制方法 |
| |
| 引用本文： | 崔乃刚,刘剑锋.微小卫星编队飞行轨道动力学及相对位置保持控制方法[J].现代防御技术,2003,31(6):33-37. |
| |
| 作者姓名： | 崔乃刚 刘剑锋 |
| |
| 作者单位： | 哈尔滨工业大学,航天工程与力学系,黑龙江,哈尔滨,150001 |
| |
| 摘 要： | 微小卫星编队飞行是20世纪90年代中、后期出现的航天新概念,它是通过一组群聚卫星的协同工作完成相应的空间任务,具有广阔的应用前景。对微小卫星编队飞行的轨道动力学建模进行了详细研究,并应用势函数方法推导了用于卫星编队飞行相对位置保持的连续控制律及离散控制律。
|
| 关 键 词： | 卫星编队 位置控制 轨道动力学方程 |
| 文章编号： | 1009-086X(2003)06-0033-05 |
| 修稿时间： | 2002年10月24 |
Small satellites formation dynamics,deployment and position-keeping control |
| |
| CUI Nai-gang,LIU Jian-feng.Small satellites formation dynamics,deployment and position-keeping control[J].Modern Defence Technology,2003,31(6):33-37. |
| |
| Authors: | CUI Nai-gang LIU Jian-feng |
| |
| Abstract: | Small satellites formation flying is a new concept about spacecrafts traveling which occurred at the end of the 20 th century.Its purpose is to make all small satellites work together and finish corresponding spacial tasks.The dynamics of a formation of small satellites is in vestigated,and the continuous control and discrete control on relative position-keeping control of small satellites formation flying by the aid of potential function are researched. |
| |
| Keywords: | Satellites formation Position control(Position-keeping) Orbital kinetic equation(Orbital dynamic equation) |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
