Akın Çatak |
Istanbul Technical University, Aerospace Research Center, 34469, Istanbul, Turkey | Esra Demir |
Istanbul Technical University, Aerospace Research Center, 34469, Istanbul, Turkey | Raziye Tekin |
Roketsan Missiles Inc., Tactical Missile Systems, Ankara, Turkey | Emre Koyuncu |
Istanbul Technical University, Aerospace Research Center, 34469, Istanbul, Turkey | İbrahim Özkol |
Istanbul Technical University, Aerospace Research Center, 34469, Istanbul, Turkey |
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Abstract:
Control over a missile's total flight time offers significant strategic advantages in military operations, including timed target engagement and orchestrated salvo attacks to boost success rates. To this end, this study introduces an innovative impact time guidance law tailored explicitly for planar engagement contexts, utilizing Bézier curves to shape the missile's range trajectory. A 4th-degree range curve is presented, from which a generalized form of the range polynomial is derived. Remarkably, our proposed guidance law aligns seamlessly with existing state-of-the-art impact time control guidance laws, thereby substantiating the efficacy and adaptability of Bézier curves in guidance law design. This alignment confirms the robust capabilities of Bézier curves as a design tool and opens new avenues for future research in developing increasingly complex and efficient guidance laws.
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