GPS-INS Fusion and Fire-Control Logic for F-7PG Jet and Harpoon Missile Systems
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Zenodo
2021
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| _version_ | 1866902196084277248 |
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| author | ZAIDI, ADNAN HAIDER |
| author_facet | ZAIDI, ADNAN HAIDER |
| contents | <p>The integration of Global Positioning System (GPS) and Inertial Navigation System (INS) technologies in avionics and fire-control systems represents a pivotal innovation in modern air-to-surface precision strike capabilities. This research presents an embedded fusion architecture tailored for the F-7PG jet, designed to interface with Harpoon missile systems via optimized Kalman filtering and legacy fire-control logic. The proposed system leverages microcontroller-based control units and analog-to-digital conversion strategies validated during the 1996–2000 timeframe. Simulation and field test validation demonstrate a circular error probable (CEP) reduction of 27%.</p> |
| format | Recurso digital |
| id | zenodo_https___doi_org_10_5281_zenodo_16417342 |
| institution | Zenodo |
| language | |
| publishDate | 2021 |
| publisher | Zenodo |
| record_format | zenodo |
| spellingShingle | GPS-INS Fusion and Fire-Control Logic for F-7PG Jet and Harpoon Missile Systems ZAIDI, ADNAN HAIDER <p>The integration of Global Positioning System (GPS) and Inertial Navigation System (INS) technologies in avionics and fire-control systems represents a pivotal innovation in modern air-to-surface precision strike capabilities. This research presents an embedded fusion architecture tailored for the F-7PG jet, designed to interface with Harpoon missile systems via optimized Kalman filtering and legacy fire-control logic. The proposed system leverages microcontroller-based control units and analog-to-digital conversion strategies validated during the 1996–2000 timeframe. Simulation and field test validation demonstrate a circular error probable (CEP) reduction of 27%.</p> |
| title | GPS-INS Fusion and Fire-Control Logic for F-7PG Jet and Harpoon Missile Systems |
| url | https://doi.org/10.5281/zenodo.16417342 |