DocumentCode
2650592
Title
H2/H∞ filtering: theory and an aerospace application
Author
Rotstein, Héctor ; Sznaier, Mario ; Idan, Moshe
Author_Institution
Dept. of Electr. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
Volume
2
fYear
1994
fDate
29 June-1 July 1994
Firstpage
1791
Abstract
In many filtering problems of practical interest, some of the noise signals satisfy the assumptions of H2 (Kalman-Bucy) filtering, while others can be more accurately modeled as bounded energy signals (hence more amenable to an H∞ filtering approach). These problems may be addressed by considering a mixed H2/H∞ filtering problem. In this paper the authors present a novel theory which solves the mixed problem exactly and in a computationally efficient way. The applicability of the theory is illustrated by designing a filter to estimate the states of an aircraft flying through a downburst.
Keywords
aircraft; discrete systems; filtering theory; linear systems; state estimation; state-space methods; H2/H∞ filtering; Kalman-Bucy filtering; aerospace application; aircraft; bounded energy signals; downburst; noise signals; Aerodynamics; Aerospace engineering; Aircraft; Equations; Filtering theory; Gaussian noise; Hydrogen; State estimation; Statistics; Wiener filter;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.752381
Filename
752381
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