面向小卫星姿态控制的磁控垂直消旋法  

A magnetorquer based vertical damping method for micro-satellite attitude control

作　　者：侯旭光[1] 晏坚[1] 靳瑾[1] 郭伟[1] 

机构地区：[1]清华大学电子工程系,100084

出　　处：《高技术通讯》2013年第11期1173-1177,共5页Chinese High Technology Letters

基　　金：国家自然科学基金(61132002)资助项目

摘　　要：针对某三轴稳定小卫星,为了避免出现非太阳能电池平面对日自旋的极端情况,提出了一种基于磁力矩器控制的垂直消旋方法,配合使用反作用飞轮,共同完成小卫星的姿态控制任务。仿真结果表明,在无轨道数据情况下该垂直消旋方法优于单纯消旋方法,整体控制方案简单有效。即使在极端情况下也能保证电源系统的稳定供电,从总体设计角度提高了小卫星的可靠性。The microsatellite attitude control was studied based on vertical damping, and a novel magnetorquer based ver tical damping method was proposed for a certain threeaxis stabilized microsatellite to avoid the occurrence of the terrible situation that the nonsolarbatteryplane spins towards the sun. In conjunction with reaction wheels, this method accomplished the satellite＇s attitude control. The simulation results show that the vertical damping method outperforms the simple damping method when no orbit information is available, and the whole attitude control scheme is simple and effective. The proposed solution guarantees a stable power supply even under the extreme situ ation, and the reliability of the whole microsatellite system.

关 键 词：姿态控制 磁力矩器 垂直消旋 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]