首页 | 本学科首页   官方微博 | 高级检索  
     检索      

关于磁强计与磁力矩器分时工作方案的研究
引用本文:黄琳,荆武兴.关于磁强计与磁力矩器分时工作方案的研究[J].航天控制,2005,23(5):37-41.
作者姓名:黄琳  荆武兴
作者单位:哈尔滨工业大学 哈尔滨150001 (黄琳),哈尔滨工业大学 哈尔滨150001(荆武兴)
摘    要:鉴于磁力矩器与磁强计同时工作会对磁强计地磁测量精度产生很大影响,本文提出一个磁强计与磁力矩器分时工作的方案,然后比较了卫星姿控系统采用不分时/分时两种方案的差异,最后研究了不同分时比例对卫星姿态控制的影响。通过仿真发现:当姿控系统采用分时方案时,电能消耗较少,早期阶段的控制精度较高,而后期稳态阶段的控制精度则相对较低;随着磁力矩器占用时间比例的下降,卫星姿态控制精度呈抛物线下降,卫星进入稳态控制阶段的时间也大大延长;分时比例存在一个相当大的范围,当在此范围内变化时,卫星姿态控制精度较高且变化幅值不大。此外,研究结果也反映出PD控制律良好的控制能力和鲁棒性。

关 键 词:磁强计  磁力矩器  分时  姿态控制  近地小卫星
文章编号:1006-3242(2005)05-0037-05
修稿时间:2005年1月11日

Research on Time-sharing Scheme for Magnetometer and Magnetorquer
Huang Lin Jing WuxingHarbin Institute of Technology,Harbin.Research on Time-sharing Scheme for Magnetometer and Magnetorquer[J].Aerospace Control,2005,23(5):37-41.
Authors:Huang Lin Jing WuxingHarbin Institute of Technology  Harbin
Institution:Huang Lin Jing WuxingHarbin Institute of Technology,Harbin 150001
Abstract:The magnetorquer used on active magnetic control small satellite would strongly disturb the geomagnetic field measurement of the magnetometer when they both were working.This paper proposed a simple time-sharing control scheme where the magnetometer and the magnetorquer worked in turn according to a certain time-sharing ratio.In this paper the performance of the attitude control system using the new time-sharing scheme is compared with that of the attitude control system using the non-time-sharing scheme.A study on how the time-sharing ratio influences the three-axis attitude control accuracy of the satellite is done.As shown in the simulations,the time-sharing scheme consumes much less power and achieves much higher accuracy of attitude control during the early phase than the non-time-sharing scheme,whereas the latter can achieve relatively lower steady-state control accuracy during the later phase.Furthermore,as the time ratio shared by the magnetorquer decreases,the attitude control accuracy takes on a parabolic decreasing trend and the satellite needs a much longer time to get into stabilization.There exists a considerable range for the time-sharing ratio,in which the attitude control accuracy of the satellite that is obtained in the case of different ratio does not change dramatically.In addition,the results also show the distinct controllability and robustness of the PD control law.Subject terms Magnetometer Magnetorquer Time-sharing Attitude control Near-Earth small satellite
Keywords:Magnetometer Magnetorquer Time-sharing Attitude control Near-Earth small satel-lite
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号