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基于非等间距采样输出的旋转矢量姿态算法

Research on Rotation Vector Attitude Algorithms Based on Non-uniform Sampling

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【作者】 葛文涛林玉荣付振宪邓正隆

【Author】 GE Wen-tao,LIN Yu-rong,FU Zhen-xian,DENG Zheng-long(Dept.of Control science and Engineering,Astronautic School,Harbin Institute of Technology,Harbin 150001,China)

【机构】 哈尔滨工业大学航天学院控制科学与工程系哈尔滨工业大学航天学院控制科学与工程系 哈尔滨150001哈尔滨150001

【摘要】 基于实际系统中陀螺的输出为非等间隔的角增量信号,重点研究了采样时刻的变化对捷联姿态算法的影响,并推导出旋转矢量三子样算法和二子样算法的通用表达式及其误差方程。传统的Miller算法已被证明是本算法的特例。研究发现,算法误差与由采样时刻构成的误差系数阵密切相关,Miller算法中的等间距采样使得该矩阵奇异,而改变采样间距可使其满秩,从而降低算法误差。然而对角增量输出的二子样算法而言,等间隔采样比非等间距采样具有更小的算法漂移。仿真及试验结果证明了本文的观点。

【Abstract】 Based on angular incremental signals from practical gyros using non-uniform sampling,the general expressions and error equations for three-sample and two-sample algorithms were presented which revealed the internal links between algorithm drift and sampling time.As a special case of our new algorithm,Miller’s algorithm error was found to be closely related to the matrix consisting of sampling points.While equal-interval sampling,on which Miller’s theory was based,could make the error matrix singular,altering the sampling intervals could render it full rank,and thereby reduced the algorithm error.However,the non-uniform sampling could increase two-sample algorithm’s error.These conclusions were confirmed by simulation and test results.

  • 【文献出处】 宇航学报 ,Journal of Astronautics , 编辑部邮箱 ,2007年04期
  • 【分类号】V448.2
  • 【被引频次】3
  • 【下载频次】165
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