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Guidance of Nonlinear Nonminimum-Phase Dynamic SystemsThe first two years research work has advanced the inversion-based guidance theory for: (1) systems with non-hyperbolic internal dynamics; (2) systems with parameter jumps; (3) systems where a redesign of the output trajectory is desired; and (4) the generation of recovery guidance maneuvers.
Document ID
19980003456
Acquisition Source
Ames Research Center
Document Type
Contractor Report (CR)
Authors
Devasia, Santosh
(Utah Univ. Salt Lake City, UT United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Subject Category
Cybernetics
Report/Patent Number
NASA/CR-97-206361
NAS 1.26:206361
Report Number: NASA/CR-97-206361
Report Number: NAS 1.26:206361
Funding Number(s)
CONTRACT_GRANT: NAG2-1042
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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