| 基于轨道机动的航天器姿态控制技术评估分析 |
| |
| 引用本文： | 肖良钢,王佳,刘震鑫.基于轨道机动的航天器姿态控制技术评估分析[J].装备指挥技术学院学报,2006,17(6):56-60. |
| |
| 作者姓名： | 肖良钢 王佳 刘震鑫 |
| |
| 作者单位： | 1. 装备指挥技术学院,试验指挥系,北京,101416
2. 装备指挥技术学院,研究生管理大队,北京,101416 |
| |
| 基金项目： | 国家高技术发展计划项目 |
| |
| 摘 要： | 实施轨道机动的航天器涉及关键技术众多,分析各项关键技术对机动效能的影响有助于确定关键技术的发展重点。主要通过仿真方法和模糊推理方法对关键技术之一的姿态控制技术进行评估分析,研究其对航天器轨道机动效能的影响。
|
| 关 键 词： | 姿态控制技术 遗传算法 模糊评估 |
| 文章编号： | 1673-0127(2006)06-0056-05 |
| 修稿时间： | 2006年2月27日 |
Evaluation Analysis on Control Technique of Attitude Based on Spacecraft Orbit Maneuver |
| |
| XIAO Lianggang,WANG Jia,LIU Zhenxin.Evaluation Analysis on Control Technique of Attitude Based on Spacecraft Orbit Maneuver[J].Journal of the Academy of Equipment Command & Technology,2006,17(6):56-60. |
| |
| Authors: | XIAO Lianggang WANG Jia LIU Zhenxin |
| |
| Abstract: | The orbit maneuvering spacecraft is related to many key technologies,which affect the operation efficiency of spacecraft.In order to identify priorities of these key technologies,it is impor- tant to analyze these key technologies infection to operation efficiency.The paper mainly evaluates the technique of attitude control by simulating and fuzzy reasoning methods so as to research its infection to operation efficiency of spacecraft. |
| |
| Keywords: | technique of attitude control genetic arithmetic fuzzy reasoning |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
