NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Closed-loop structural stability for linear-quadratic optimal systemsAn explicit parametrization of a subclass of linear constant gain feedback maps that never destabilize an originally open-loop stable system is presented. These results are used to obtain several new structural stability results for multiinput linear-quadratic feedback optimal designs.
Document ID
19770015872
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wong, P. K. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Athans, M. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Ames Res. Center Systems Reliability Issues for Future Aircraft
Subject Category
Cybernetics
Accession Number
77N22816
Funding Number(s)
CONTRACT_GRANT: NGL-22-009-124
CONTRACT_GRANT: AF-AFOSR-2273-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19770015864Collected WorksSystems reliability issues for future aircraft
No Preview Available