Numerical analysis of dynamics of an automatically tracked anti-tank guided missile using polynomial functions

• Autorzy: Koruba Z. , Nocoń Ł.

Identyfikatory

DOI

10.15632/jtam-pl.54.1.13

• Języki publikacji: EN

Abstrakty

EN

The paper presents algorithms of automatic control of an intelligent anti-tank guided missile (ATGM) with possibility of attacking the target from the upper ceiling and with possibility of the missile flight through indicated points in space. The polynomial functions are used to designate the program trajectories. Numerical analysis of the operation of chosen algorithms is performed. The results are presented in a graphical form. As it results from the conducted tests, the proposed algorithms of automatic control of ATGM with the use of polynomial functions work properly during attack on the target from the upper ceiling, for both mobile and immobile targets.

Słowa kluczowe

EN

homing; direction algorithm; anti-tank guided missile

• Wydawca: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
• Czasopismo: Journal of Theoretical and Applied Mechanics
• Rocznik: 2016
• Tom: Vol. 54 nr 1
• Strony: 13--25
• Opis fizyczny: Bibliogr. 13 poz., rys.

Twórcy

autor

Koruba Z.

• Kielce University of Technology, Faculty of Mechatronics and Machine Design, Kielce, Poland

autor

Nocoń Ł.

• Kielce University of Technology, Faculty of Mechatronics and Machine Design, Kielce, Poland

Bibliografia

• 1. Baranowski L., 2013, Equations of motion of spin-stabilized projectile for flight stability testing, Journal of Theoretical and Applied Mechanics, 51, 1, 235-246
• 2. Evans D.M., 1990, The direct-fire anti-armour capability of UK land forces, Intern, Defense Review, 7, 739-742
• 3. Gapiński D., Stefański K., 2014, Modified optical scanning and tracking head for identification and tracking air targets, Solid State Phenomena, 210, 145-155, DOI: 10.4028/www.scientific.net/SSP.210.145
• 4. Grzyb M., Koruba Z., 2011, Guiding a bomb to a sea target (in Polish), Research Journal of Polish Naval Academy, 185A, ISSN 0860-889X, 189-195
• 5. Harris J., Slegers N., 2009, Performance of a fire-and-forget anti-tank missile with a damaged wing, Mathematical and Computer Modelling, 50, 1/2, 292-305
• 6. Koruba Z., 2008, The Elements of the Theory and Applications of the Controlled Gyroscope (in Polish), Monographs, Studies, Dissertations M7, Kielce University of Technology, Kielce
• 7. Koruba Z., Nocoń Ł., 2012, Selected algorithms of automatic guidance of anti-tank missiles attacking targets from upper ceiling (in Polish), Pomiary, Automatyka, Robotyka, 2
• 8. Koruba Z., Osiecki J., 2006, Structure, Dynamics and Navigation of Chosen Precision Kill Weapons, Publishing House of Kielce University of Technology, ISBN 83-88906-17-8, Kielce, 50-209
• 9. Krzysztofik I., 2012, The dynamics of the controlled observation and tracking head located on a moving vehicle, Solid State Phenomena, 180, 313-322, ISSN 1012-0394, DOI: 10.4028/www.scientific.net/SSP.180.313
• 10. Nocoń Ł., 2013, Detection control system of a missile safe distance trajectory, Proceedings of the 10th European Conference of Young Researchers and Scientists, EDIS – Żilina University Publisher, ISBN 978-80-554-0694-7, Transcom 2013, Żylina, 139-142
• 11. Nocoń Ł., Stefański K., 2014, The analysis of anti-tank rocket dynamics including external disturbances (in Polish), [In:] Mechanika w Lotnictwie, ML-XVI 2014, K. Sibilski (edit.), PTMTS Warsaw, ISBN 978-83-932107-3-2, 409-426
• 12. Siouris G.M., 2004, Missile Guidance and Control Systems, Springer, New York
• 13. Yanushevsky R., 2008, Modern Missile Guidance, CRC Press Taylor & Francis Group, New York

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniajacą naukę.