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Constrained optimal controller for linear systems with state and control dependent disturbanceThe problem is posed with the additional constraints that the dynamic controller uses only noise-corrupted outputs, and that its dimension is significantly lower than that of a Kalman filter. The unknown disturbance is viewed as an adversary which tries to maximize a performance criterion: a criterion that the controller gains attempt to minimize. The optimal controller gains are determined by solving a nonlinear matrix two-point boundary value problem.
Document ID
19750006423
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Basuthakur, S.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Cybernetics
Report/Patent Number
NASA-TN-D-7763
G-7445
Report Number: NASA-TN-D-7763
Report Number: G-7445
Accession Number
75N14495
Funding Number(s)
PROJECT: RTOP 630-21-75-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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