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飞行试验数据的相容性检验和数据重建 被引量:1

COMPATIBILITY CHECK OF THE FLIGHT TEST DATA AND RECONSTRUCTION OF THE DATA
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摘要 本文采用飞行器六自由度运动方程组,建立了飞行试验数据相容性检验的数学模型.应用最大似然估计求得测量数据的系统误差并进行数据重建。利用计入测量噪音的六自由度动力学方程组的仿真数据检查了方法的可行性和程序的正确性,最后处理各种飞行器的飞行试验数据,得到了满意的结果. In this paper, the mathematical model of compatibility check of flight test date is set up based on the kinematic equations with six freedom of aircraft. By using the maximum likelihood method the system error of the measurement data can be obtained and the flight data can be reconstructed. The feasibility of the method and the correctness of the program have been checked using the simulation data calculated by six freedom kinematic equations in consideration of the measurement noice. Finally various flight test data are processed and the results are quite satisfactory.
出处 《飞行力学》 CSCD 北大核心 1989年第1期62-71,共10页 Flight Dynamics
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  • 1汪清 何开锋 和争春.跨大气层飞行器气流参数的测量与估计方法[J].载人航天,2004,2:31-35.
  • 2MULDER J A,CHU Q P,SRIDHAR J K,BREEMAN J H,LABAN M.Non-linear aircraft flight path reconstruction review and new advances[J].Progress in aerospace science,1999,35:673-726.
  • 3KLEIN V,SCHIESS J R.Compatibility check of measured aircraft responses using kinematic equation and Extended Kalman Filter[R].NASA TN D-8514,1977.
  • 4EVANS R J,GOODWIN G C,FEIK R A,MARTIN C,LOZANO-LEAL R.Aircraft data compatibility checking using maximum likelihood and Extended Kalman Filter estimation[A].Proceedings of 7th IFAC Symposium on Identification and System Parameter Estimation [C],1985,487-492.
  • 5MAINE R E,ILIFF K W.Formulation of a practical algorithm for parameter estimation with process and measurement noise[A].Proceedings of 6th IFAC Symposium on Identification and System Parameter Estimation[C],1982,1139-1144.

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