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Multi-input, multi-output regulator design for constant disturbances and non-zero set points with application to automatic landing in a crosswindUndesirable steady offsets result when a stationary, linear regulator using state feedback is subjected to constant disturbances and/or non-zero setspoints. To eliminate these offsets, the disturbances and non-zero setpoints can be fed forward to the control. Only when the number of outputs is less than or equal to the number of control inputs can the outputs be maintained at arbitrary non-zero setpoints. The state and the disturbance may be estimated using a constant gain Kalman filter or by modeling the constant disturbances as exponentially correlated processes with long correlation times.
Document ID
19740007265
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Holley, W. E.
(Stanford Univ. CA, United States)
Bryson, A. E., Jr.
(Stanford Univ. CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1973
Subject Category
Navigation
Report/Patent Number
SUDAAR-465
NASA-CR-136618
Report Number: SUDAAR-465
Report Number: NASA-CR-136618
Accession Number
74N15378
Funding Number(s)
CONTRACT_GRANT: NGL-05-020-007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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