Simulation study of a missile cold launch system

• Autorzy: Głębocki R. , Jacewicz M.

Identyfikatory

DOI

10.15632/jtam-pl.56.4.901

• Języki publikacji: EN

Abstrakty

EN

In this paper the missile flight dynamics during the launch phase is studied. The main concept behind this work was to use a vertical cold launch system and the rapid pitch maneuver to achieve longer missile range and better firing coverage. A set of a small pulse rocket engines was used to obtain the desired missile attitude. The physical and mathematical models of the missile are described. The pulse jets control algorithm is presented. The computer program of the missile model has been developed in the Simulink environment. The missile behavior in the low-speed flight envelope has been examined. The results of numerical simulations in the form of the graphs are presented. It has been obtained that there exist several benefits of the cold launch method as increased range and higher target kill probability.

Słowa kluczowe

EN

guided missile; modeling; simulation

• Wydawca: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
• Czasopismo: Journal of Theoretical and Applied Mechanics
• Rocznik: 2018
• Tom: Vol. 56 nr 4
• Strony: 901—913
• Opis fizyczny: Bibliogr. 14 poz., rys.

Twórcy

autor

Głębocki R.

• Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Warsaw, Poland

autor

Jacewicz M.

• Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Warsaw, Poland

Bibliografia

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• 2. Blakelock J., 1991, Automatic Control of Aircraft and Missiles, New York, NY, John Wiley & Sons, Inc.
• 3. Despirito J., 2013, Lateral Reaction Jet Flow Interaction Effects on a Generic Fin-Stabilized Munition in Supersonic Crossflow, Army Research Laboratory
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• 6. Maher K., 2002, PRODAS V3 – Technical Manual, Arrow Tech
• 7. MBDA Systems, 2014, MBDA – Common Anti-air Modular Missile (CAMM), Retrieved from https://youtu.be/Nnb20mrT1kw
• 8. TOR-M1 9A331 (SA-15 Gauntlet) surface-to-air missile, 2012, Retrieved from https://www.youtube.com/watch?v=qcC0rXxXVNA
• 9. Weinacht P., 2004, Lateral Control Jet Aerodynamic Predictions for a 2.75-in Rocket Testbed Munition, Army Research Laboratory
• 10. Yuhang W., Yu Y., Kemao M., 2006, Lateral thrust and aerodynamics blended control system fesign based on variable structure model following, Intelligent Control and Automation, Dalian, 8183-8186
• 11. Zarchan P., 2012, Tactical and Strategic Missile Guidance, American Institute of Aeronautics and Astronautics
• 12. Zhen S., Wenqiao M., Yufang Z., Huichao H., 2012, Lateral thrust and aerodynamics compound control system of missile based on adaptive fuzzy control, Computational Intelligence and Design (ISCID), Hangzhou
• 13. Zipfel P., 2007, Modeling and Simulation for Aerospace Vehicle Dynamics, American Institute of Aeronautics and Astronautics
• 14. Żugaj M., Głębocki R., 2010, Model of gasodynamic control system for guided bombs, Journal of Theoretical and Applied Mechanics, 48, 1, 27-44

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).