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内编队重力场测量卫星全推力姿轨一体化控制研究 被引量：3

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摘要 内编队重力场测量卫星作为一种新概念的纯引力轨道飞行器,通过精密定轨和相对状态测量实现高精度地球重力场测量.其中对外卫星的控制保持编队内卫星在纯引力轨道上稳定飞行是决定测量水平的关键因素之一.针对稳态工作模式的内编队系统,研究了仅用推力器实现姿态轨道一体化控制的问题,构建了姿态非线性和共用推力器引起的姿态轨道耦合的六自由度平动和转动动力学模型,并基于约束非线性模型预测技术建立了姿轨一体化控制的二次型优化模型.通过仿真实验可知,约束非线性模型预测控制方法计算快速,能克服部分约束条件的非凸性;推力器布局合理,推力消耗低,满足内编队系统任务需求.
作者 吉莉 刘昆 项军华
机构地区 国防科技大学航天与材料工程学院
出处 《中国科学：技术科学》 EI CSCD 北大核心 2012年第2期220-229,共10页 Scientia Sinica(Technologica)
关键词 重力场测量卫星 内编队系统 姿轨一体化控制 模型预测控制
分类号 V448.2 [航空宇航科学与技术—飞行器设计]
  • 相关文献

参考文献18

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共引文献114

同被引文献23

  • 1王佐磊,薛大同,唐富荣.静电悬浮加速度计敏感结构的热噪声分析[J].真空与低温,2005,11(2):83-89. 被引量：12
  • 2陈光锋,唐富荣,薛大同.静电悬浮加速度计气体阻尼及其对控制系统特性影响分析[J].真空与低温,2005,11(4):216-221. 被引量：7
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引证文献3

二级引证文献7

中国科学：技术科学
2012年 第2期

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