Unsaturated Optimal Guidance Law for Impact Angle and Acceleration Constraints

Most research on impact angle control has not addressed acceleration constraints, as it assumes that maneuverability is sufficient. However, when guidance commands are saturated due to aerodynamic or structural loads, the miss distance and impact angle errors can be significantly large. This paper p...

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Bibliographic Details
Main Authors: Junseong Kim, Sungjin Cho
Format: Article
Language:English
Published: IEEE 2023-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/10283815/