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CEAS EuroGNC 2026 |
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Midcourse Guidance Based on Augmented Pursuit Guidance for Ducted-Rocket Missiles |
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| Abstract: This paper proposes an Augmented Pursuit Guidance (APG)-based guidance law that faithfully tracks optimal trajectories by reproducing the optimal lead angle history with respect to the target. Although optimal guidance laws offer theoretical performance advantages, their real-time applicability is often limited due to computational complexity. To address this gap, the proposed APG method provides a practical and implementable alternative that closely approximates the optimal solution using precomputed or polynomial-approximated data. Simulation study shows that APG is a simple and efficient method for trajectory tracking during the mid-course guidance phase of a long-range air-to-air missile equipped with a dual-pulse rocket. | ||||||||
| Keywords: Midcourse Guidance; Trajectory Following; Arrival Time Control; Pursuit Guidance | ||||||||
| Min-Jea Tahk, Boseok Kim, Dain Jeong, Chang-Hun Lee: Midcourse Guidance Based on Augmented Pursuit Guidance for Ducted-Rocket Missiles. Proceedings of the 2026 CEAS EuroGNC conference. Madrid, Spain. May 2026. doi: 10.82124/CEAS-GNC-2026-016. |
| BibTeX entry (UTF-8): @Incollection{CEAS-GNC-2026-016, author = {Tahk, Min-Jea and Kim, Boseok and Jeong, Dain and Lee, Chang-Hun}, title = {Midcourse Guidance Based on Augmented Pursuit Guidance for Ducted-Rocket Missiles}, booktitle = {Proceedings of the 2026 {CEAS EuroGNC} conference}, address = {Madrid, Spain}, month = may, year = {2026}, doi = {10.82124/CEAS-GNC-2026-016} } |