DocumentCode
794367
Title
Methods for injection-error analysis and their comparison
Author
Irwin, John D. ; Hung, James C.
Author_Institution
University of Tennessee, Knoxville, TN, USA
Volume
12
Issue
3
fYear
1967
fDate
6/1/1967 12:00:00 AM
Firstpage
276
Lastpage
281
Abstract
Statistical techniques for the analysis of missile injection errors are studied in detail. The commonly used direct and adjoint methods are reviewed and extended. It is shown that the determination of the covariance matrix is equivalent to the determination of two transformation matrices for both methods. In general, the adjoint method is more efficient. But for a special case the direct method could be preferable depending upon the relative dimension of the system state and the error source. Two examples are given to verify the results. The techniques presented can be applied equally well to a wide variety of control system problems.
Keywords
Linear systems, time-varying continuous-time; Missile guidance; Computer errors; Control systems; Covariance matrix; Engines; Fuels; Hardware; Milling machines; Missiles; Space vehicles; Uncertainty;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1967.1098598
Filename
1098598
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