Using the MATLAB.SIMULINK software suite for ballistic analysis

Authors: Nikanorova M.D., Vedenichev I.V.
Published in issue: #10(15)/2017
DOI: 10.18698/2541-8009-2017-10-183
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control
Keywords: MATLAB.Simulink environment, ballistics, numerical simulation, correcting filters
Published: 04.10.2017

In this work we have simulated the flight of the material point in the MATLAB.Simulink environment coded in С++ and analyzed the results obtained. The benefits of applying this software suite have been revealed. We simulated the flight of the ideally homing surface-to-air missile and the surface-to-air missile real flight. The article proves the impossibility of using the guidance system without the correcting filters.

References

[1] Vedenichev I.V., Lysikova V.S. Research on effect of director cone matrix calculation algorithm on numerical simulation results of aircraft movement. Molodezhnyy nauchno-tekhnicheskiy vestnik, 2016, no. 10. Available at: http://sntbul.bmstu.ru/doc/850294.html.

[2] German-Galkin S.G. MATLAB & Simulink. Proektirovanie mekhatronnykh sistem na PK [MATLAB & Simulink. Computer programming of mechatronics systems]. Sankt-Petersburg, KORONA-Vek publ., 2008, 368 p.

[3] Ilyukhin S.N., Moskalenko V.O., Khlupnov A.I. Experimentally studied influence of the bullet head shape on dispersion characteristics at subsonic airspeeds. Aerokosmicheskiy nauchnyy zhurnal [Aerospace scientific journal], 2015, no. 5, pp. 38–48. Available at: http://aerospace.elpub.ru/jour/article/view/27.

[4] Emel’yanova N.S. Software for experimental research on ballistic track. Molodezhnyy nauchno-tekhnicheskiy vestnik, 2014, no. 6. Available at: http://sntbul.bmstu.ru/doc/723443.html.

[5] Alekseev E.R., Chesnokova O.V. Reshenie zadach vychislitel’noy matematiki v paketakh Mathcad 12, MATLAB 7, Maple 9 [Solving problem of computational mathematics in Mathcad 12, MATLAB 7, Maple 9 software packages]. Moscow, NT Press publ., 2006, 496 p.

[6] Ilyukhin S.N., Benevol’skiy S.V., Grabin V.V. Formirovanie oblika zenitnoy upravlyaemoy rakety i dinamicheskiy analiz ee sistemy upravleniya [Forming conception of guided air defense rocket and dynamic analysis of its control system]. Moscow, Bauman Press, 2012, 80 p.

[7] Ilyukhin S.N. Synthesis of pointing system and stabilization loop using log-magnitude and phase diagram method through the example of guided air defense rocket arbitrary model. Molodezhnyy nauchno-tekhnicheskiy vestnik, 2012, no. 7. Available at: http://sntbul.bmstu.ru/doc/467279.html.

[8] Afonin V.V. Modelirovanie system [System modelling]. Moscow, BINOM. Laboratoriya znaniy publ., 2010, 231 p.