NASA NTRS · 19980003456
Guidance of Nonlinear Nonminimum-Phase Dynamic Systems
Abstract
The 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.
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Devasia, Santosh. 1997-01-01. Guidance of Nonlinear Nonminimum-Phase Dynamic Systems. https://ntrs.nasa.gov/citations/19980003456
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