北京航空航天大学学报 ›› 2008, Vol. 34 ›› Issue (12): 1437-1440.

• 论文 • 上一篇    下一篇

基于混合Gramian的柔性航天器保结构平衡降阶

孟占峰, 韩 潮   

  1. 北京航空航天大学 宇航学院, 北京 100191
  • 收稿日期:2007-12-17 出版日期:2008-12-31 发布日期:2010-09-16
  • 作者简介:孟占峰(1980-),男,北京人,博士生,mengzf@gmail.com.

Structure-preserving balanced truncation for flexible spacecraft using cross Gramian

Meng Zhanfeng, Han Chao,   

  1. School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
  • Received:2007-12-17 Online:2008-12-31 Published:2010-09-16

摘要: 对于柔性航天器动力学方程的降阶问题,传统的内平衡降阶方法破坏了原方程的动力学结构.为了解决这一问题,提出了一种牺牲严格内平衡状态,而保留原系统动力学特性的近似内平衡降阶方法.该方法利用混合Gramian描述系统的模态价值,针对柔性航天器动力学方程的特殊形式,给出了混合Gramian的闭合解析解.该方法得到的降阶模型可以保留原系统包括二阶结构,对称和正定性在内的所有动力学特性.数值算例表明该方法不但可以达到与传统一阶内平衡方法相当的降阶精度,而且降阶速度有大幅度提升.

Abstract: For model reduction of flexible spacecraft, conventional first-order balanced truncation(FOBT) method will destroy the second-order structure and dynamic properties of original system. In order to overcome this drawback, a new structure-preserving approximated balanced truncation method for model reduction of flexible spacecraft was proposed. The modal cost was described by a cross Gramian and the closed-form solution of cross Gamian was obtained via special form of dynamical equation of flexible spacecraft. The new method preserves the second-order structure, symmetry and positive definiteness of the original system. The numerical results show that the new method is superior to conventional first-order balanced truncation(FOBT) method for improving efficiency without sacrificing accuracy.

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