A modified input-output feedback linearization guidance law adds a zero-dynamics correction to ensure LOS alignment produces a closing trajectory and interception for a broad class of initial conditions.
Circumventing un stable zero dynamics in input-output linearization of long itudinal flight dynamics
1 Pith paper cite this work. Polarity classification is still indexing.
1
Pith paper citing it
fields
eess.SY 1years
2026 1verdicts
UNVERDICTED 1representative citing papers
citing papers explorer
-
Feedback Linearization-Based Guidance with Zero-Dynamics Correction for Guaranteed Interception
A modified input-output feedback linearization guidance law adds a zero-dynamics correction to ensure LOS alignment produces a closing trajectory and interception for a broad class of initial conditions.