Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle
By Hangju Cho, Chang-Kyung Ryoo, Antonios Tsourdos, Brian A. White. 2014
79 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computer Vision and Pattern Recognition
View Paper: https://www.semanticscholar.org/paper/5753c0b3958a79036d3727ab58fd67e3f368b4c3
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In Aerospace Engineering
In Computer Vision and Pattern Recognition
Citations in the corpus
- Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law (2015, methodology): “The concept of zero-effort collision triangle was introduced in [19], and an impact-angle control optimal guidance law was developed for missiles with arbitrary velocity profiles against maneuvering targets based on the linearization of kinematics around the zero-effort collision triangle.”