IDENTIFICATION OF OBSERVER KALMAN FILTER MARKOV PARAMETERS - THEORY AND EXPERIMENTS

被引:279
作者
JUANG, JN [1 ]
PHAN, M [1 ]
HORTA, LG [1 ]
LONGMAN, RW [1 ]
机构
[1] COLUMBIA UNIV,NEW YORK,NY 10027
关键词
D O I
10.2514/3.21006
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper discusses an algorithm to compute the Markov parameters of an observer or Kalman filter from experimental input and output data. The Markov parameters can then be used for identification of a state-space representation, with associated Kalman or observer gain, for the purpose of controller design. The algorithm is a nonrecursive matrix version of two recursive algorithms developed in previous works for different purposes, and the relationship between these other algorithms is developed. The new matrix formulation here gives insight into the existence and uniqueness of solutions of certain equations and offers bounds on the proper choice of observer order. It is shown that if one uses data containing noise and seeks the fastest possible deterministic observer, the deadbeat observer, one instead obtains the Kalman filter, which is the fastest possible observer in the stochastic environment. The results of the paper are demonstrated in numerical studies and experiments on the Hubble space telescope.
引用
收藏
页码:320 / 329
页数:10
相关论文
共 15 条
[1]   INTEGRATED SYSTEM-IDENTIFICATION AND STATE ESTIMATION FOR CONTROL OF FLEXIBLE SPACE STRUCTURES [J].
CHEN, CW ;
HUANG, JK ;
PHAN, M ;
JUANG, JN .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (01) :88-95
[2]  
GAWRONSKI W, 1990, ADV LARGE SCALE SYST, P143
[3]   SINGLE-MODE PROJECTION FILTERS FOR MODAL PARAMETER-IDENTIFICATION FOR FLEXIBLE STRUCTURES [J].
HUANG, JK ;
JUANG, JN ;
CHEN, CW .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1989, 12 (04) :568-576
[4]  
JUANG JN, 1988, CONTR-THEOR ADV TECH, V4, P5
[5]   AN EIGENSYSTEM REALIZATION-ALGORITHM FOR MODAL PARAMETER-IDENTIFICATION AND MODEL-REDUCTION [J].
JUANG, JN ;
PAPPA, RS .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1985, 8 (05) :620-627
[6]  
JUANG JN, 1990, MECHANICS CONTROL LA, V129, P87
[7]  
JUANG JN, 1990, P AIAA GUID NAV CONT, P1361
[8]  
JUANG JN, 1990, NASA TM102666
[9]  
JUANG JN, 1988, SHOCK VIBRATION DIGE, V20, P4
[10]  
JUANG JN, 1992, NASA TM107566