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What is Differential Geometric Missile Guidance about?

This paper introduces a new differential geometric guidance methodology for the impact-time control (ITC) problem in missile guidance, specifically for constant-speed missiles. It develops a circular predictive guidance (CPG) law that utilizes a simple circular arc guidance equation and incorporates a dual-virtual-target (DVT) concept to guide missiles effectively without needing time-to-go estimations or numerical iterations. The proposed strategies aim to enhance missile engagement capabilities while mini

Author

anhgaham

Language

EN