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Identification of observer/Kalman filter Markov parameters - Theory and experimentsAn algorithm to compute Markov parameters of an observer or Kalman filter from experimental input and output data is discussed. The Markov parameters can then be used for identification of a state space representation, with associated Kalman gain or observer gain, for the purpose of controller design. The algorithm is a non-recursive matrix version of two recursive algorithms developed in previous works for different purposes. 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 gives 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. Results are demonstrated in numerical studies and in experiments on a ten-bay truss structure.
Document ID
19910065070
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Juang, Jer-Nan
(NASA Langley Research Center Hampton, VA, United States)
Phan, Minh
(NASA Langley Research Center Hampton, VA, United States)
Horta, Lucas G.
(NASA Langley Research Center Hampton, VA, United States)
Longman, Richard W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 91-2735
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: New Orleans, LA
Country: United States
Start Date: August 12, 1991
End Date: August 14, 1991
Accession Number
91A49693
Distribution Limits
Public
Copyright
Other

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