航空学报 > 1993, Vol. 14 Issue (1): 80-84

导弹飞行数据的相容性检验研究

李乃宏, 吴瑶华, 崔平远, 杨涤   

  1. 哈尔滨工业大学航天学院, 哈尔滨 150006
  • 收稿日期:1990-05-01 修回日期:1992-02-25 出版日期:1993-01-25 发布日期:1993-01-25

A STUDY ON COMPATIBILITY CHECK MISSILE FLIGHT TEST DATA

Li Nai-hong, Wu Yao-hua, Cui Pmg-yuan, Yang Di   

  1. School of Astronautics, Harbin Institute of Technology, Harbin, 150006
  • Received:1990-05-01 Revised:1992-02-25 Online:1993-01-25 Published:1993-01-25

摘要: 本文针对导弹飞行试验的特点,采用导弹六自由度动力学方程建立了飞行数据相容性检验的数学模型。在有舵偏激励同时考虑偏差间相关性的条件下,应用广义Kalman滤波方法进行常值及比例因子偏差的估计。仿真及实际应用表明所建数学模型及估计方法正确有效,所得结果与由高速可重复模拟匹配技术结果极为接近。

关键词: 数据相容性检验, 广义Kalman滤波, 飞行试验, 模拟匹配技术

Abstract: An efficient method for flight test data analysis would be to determine first whether the data channels are all compatible, make whatever adjustment required, and then use the refined compatible data for aerodynamic parameter estimation. In this paper, by considering the characteristics of missle flight tests, a model for the compatibility check of measured missile response is presented. On the condition of designing input signal and considering the correlation among bias errors, by using extended Kalman filter, simulation and practical application indicate that the mathematical model being set up and the estimation algorithm are reasonable and valid. The obtained results are very close to those determined by high-speed repetitive operation analog matching, and the effectiveness of the results is proved once again.

Key words: data compatibility check, extended Kalman filter, fight test, analog matching tech-pique