Abstract
This paper presents some introductory results from simulations of the surface-to-air missile which uses aerodynamic and lateral jet blended control. The designed projectile is equipped in a set of small rocket engines which can produce lateral forces. The influence of various control parameters on missile flight dynamics were studied. It was obtained that presented method of control improves significantly missile maneuverability. Shorter response times and better projectile accuracy were achieved when compared only to pure aerodynamic control. Simulation results in form of graphs are presented and discussed. The results, which were obtained, may be used in further stages of autopilot design process.
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Głębocki, R., Jacewicz, M., Ożóg, R. (2018). Some Problems of Aerodynamic and Lateral-Jet Blended Control for the Surface-to-Air Missile. In: Szewczyk, R., Zieliński, C., Kaliczyńska, M. (eds) Automation 2018. AUTOMATION 2018. Advances in Intelligent Systems and Computing, vol 743. Springer, Cham. https://doi.org/10.1007/978-3-319-77179-3_29
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DOI: https://doi.org/10.1007/978-3-319-77179-3_29
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