采用信标的大型可展开天线指向控制方法  

Pointing Control of Large Deployable Antenna Based on Beacon

作　　者：邢志钢[1] 刘丽坤[2] 郑钢铁[1] 周志成[2] 

机构地区：[1]清华大学航天航空学院,北京100084 [2]中国空间技术研究院通信卫星事业部,北京100094

出　　处：《中国空间科学技术》2012年第3期1-6,14,共7页Chinese Space Science and Technology

基　　金：装备预研基金(9140A20020610HT0506)重点资助项目

摘　　要：为提高大型可展开天线的指向控制精度,并适应喷气卸载等在轨工况,基于Craig-Bampton法建立了表征柔性天线指向的动力学模型,在此基础上提出了一种采用信标的大天线指向控制方法。该方法先基于卡尔曼滤波,对大天线的振动状态进行检测,若天线未出现明显振动,则通过信标敏感器修正天线指向偏差,同时引入星本体姿态敏感器以保证稳定性;若天线振动超过阈值,则仅引入星本体敏感器以衰减振动,直至天线未出现明显振动。最后利用瑟拉亚(Thuraya)卫星的在轨实测热变形数据进行了仿真验证。结果表明,在未受到喷气扰动时,大天线指向精度优于±0.02°,在受到喷气扰动后,系统可正确检测并切换跟踪输入。这说明,该指向控制方法在保证稳定性的同时,可以有效修正大天线指向偏差,并能适应在轨位保、卸载喷气工况。Abstract In order to increase to on-orbit conditions such as jet pointing accuracy of the large dumping, the Craig-Bampton antenna pointing dynamic modeling, and a pointing control method By using Kalman filter, the flexible antenna vibration status was deployable antenna and adapt modal synthesis was used in based on beacon was proposed. estimated. If the antennas donot vibrate obviously, the antenna pointing was adjusted by beacon sensors, and the stability was ensured by collocated attitude sensors. While the antenna vibration exceeds the threshold, only the collocated attitude sensors were induced to attenuate oscillation until vibration was attenuated. By using the in orbit thermal deformation testing data of the Thuraya satellite, the simulation results show that the antenna pointing accuracy without jet is superior to ±0. 02°, and the vibration could be estimated correctly with the switch of tracking input after jet dumping. The results indicate that the antenna pointing error is adjusted with the guarantee of stability, and the influences of jet dumping and station-keeping are limited with the proposed vibration estimation method.

关 键 词：信标敏感器 天线指向控制 姿态动力学 指向精度 大型可展开天线 

分 类 号：V443.4[航空宇航科学与技术—飞行器设计]