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应用科学学报 ›› 2010, Vol. 28 ›› Issue (2): 209-215.

• 控制与系统 • 上一篇    下一篇

基于大气阻力的微小卫星编队控制

  

  1. 1. 南京航空航天大学自动化学院，南京210016
    2. 南京航空航天大学航天学院，南京210016
    3. 南京航空航天大学高新技术研究院，南京210016
  • 收稿日期:2009-07-01 修回日期:2009-10-30 出版日期:2010-03-30 发布日期:2010-03-30
  • 作者简介:陈志明，博士生，研究方向：卫星编队飞行及任务管理，E-mail: zenkichen@gmail.com; 王惠南，教授，博导，研究方向：GPS、惯导及精密仪器，E-mail: whn@nuaa.edu.cn

Satellite Formation Fly Control Based on Atmospheric Drag

  1. 1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016, China
    2. College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    3. Academy of Frontier Sciences, Nanjing University of Aeronautics and Astronautics,Nanjing 210016, China
  • Received:2009-07-01 Revised:2009-10-30 Online:2010-03-30 Published:2010-03-30
  • Supported by:

    教育部博士点专项科研基金(No.20070287007)资助

PDF

1848

被引次数

2

摘要：

以传统卫星编队及姿态控制方案为基础，提出一种基于大气阻力的微小卫星编队飞行控制方案，给出相应的系统配置和姿态轨道控制律. 该方案采用4 块气动板对卫星姿态及队形进行控制，提高了功能密度，显著减小了系统复杂性. 采用气动板使卫星编队飞行任务摆脱卫星燃料载量的限制，延长了卫星的生命周期，在应用中具有优势. 仿真实验验证了基于大气阻力的卫星控制方案的有效性.

关键词: 大气阻力, 卫星编队, 姿态控制, 队形控制

Abstract:

A new control method is described using atmospheric drag. It was based on the traditional control method of  satellite formation flying. Besides, the system configuration and control law are given. With drag panels, fuel is no longer a limitation to the satellite service life. This method is useful both in attitude control and formation control problems. It can reduce system complexity and enhance function density, and therefore has a good application prospect. Simulation results show that the method is effective in terms of the expected control efficiency.

Key words: atmospheric drag, satellite formation, attitude control, formation control

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