系统工程与电子技术

• 制导、导航与控制 • 上一篇    下一篇

改进的强跟踪飞机舵面快速故障诊断方法

马骏, 倪世宏, 解武杰, 董文瀚   

  1. 空军工程大学航空航天工程学院, 陕西 西安 710038
  • 出版日期:2015-10-27 发布日期:2010-01-03

Fast fault diagnosis of improved strong tracking aircraft actuator

MA Jun, NI Shi-hong, XIE Wu-jie, DONG Wen-han   

  1. Aeronautics and Astronautics Engineering Institute, Air Force Engineering University, Xi’an 710038, China
  • Online:2015-10-27 Published:2010-01-03

摘要:

针对多模型自适应估计(multiple model adaptive estimation, MMAE)方法适应突变故障能力差、多重渐消因子强跟踪算法滤波发散、故障条件概率计算量大等问题,提出一种改进的多重渐消因子强跟踪多模型自适应估计(strong tracking multiple model adaptive estimation, STMMAE)快速故障诊断方法。通过多重渐消因子提高了故障突变时滤波器的跟踪性能;通过改进一步预测协方差阵更新方程,保证了滤波器稳定性,提高了估计精度;采用基于欧几里得范数的飞机舵面故障概率快速计算方法,降低了故障概率计算量。对比仿真表明,该算法跟踪性强、速度快、精度高,具有较好的鲁棒性和稳定性。

Abstract:

The multiple model adaptive estimation(MMAE) method has low capability to track abrupt faults, therefore multiple  fading factors may result in diverging the strong tracking filter(STF). Moreover, the fault probability calculation is large. An improved strong tracking multiple model adaptive estimation (STMMAE) fast diagnosis algorithm is proposed. The tracking performance of the filter is improved by multiple fading factors. An improved renewal equation of the step prediction covariance matrix is proposed. The stability of the filter is guaranteed, and the estimation accuracy is improved. Based on the Euclidean norm, a fast fault isolation method which reduces the fault probability calculation is proposed. The simulation results show that the proposed algorithm is more efficient and has a better performance.