Have a personal or library account? Click to login

Study for a 122 mm Artillery Rocket Steered with Lateral Thrusters

Open Access
|Jul 2025

References

  1. Harkins T.E., and Brown T.G. Using Active Damping as a Precision Enhancing Technology for 2.75 inch Rockets, ARL-TR-1772, Army Research Laboratory, USA, 1999.
  2. Jitpraphai T., and Costello M. Dispersion Reduction of a Direct Fire Rocket Using Lateral Pulse Jets, ARL-CR-465, Army Research Laboratory, USA, April 2001.
  3. Jitpraphai T., and Costello M. Dispersion Reduction of a Direct Fire Rocket Using Lateral Pulse Jets, Journal of Spacecraft and Rockets, Vol. 38, No. 6, November-December 2001, pp. 929-936.
  4. Gupta S.K., Saxena S., and Ghosh A.K. On Implementation of Trajectory Correction System on a Routinely Used Artillery Rocket, AIAA 2006-6007, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Keystone, CO, USA, August 21-24, 2006.
  5. Gupta S.K., Saxena S., Singhal A., and Ghosh A.K. Trajectory Correction Flight Control System using Pulsejet on an Artillery Rocket, Defence Science Journal, Vol. 58, No. 1, January 2008, pp. 15-33.
  6. Pavkovic B. Research of Projectile Trajectory Correction Methods in Function of Their Range and Precision Enhancement, PhD thesis, University of Belgrade, Serbia, 2012.
  7. Pavkovic B., Pavic M., and Cuk D. Frequency-Modulated Pulse-Jet Control of an Artillery Rocket, Journal of Spacecraft and Rockets, Vol. 49, No. 2, March-April 2012, pp. 286-294.
  8. Gao M., Zhang Y., and. Yang S. Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles, International Journal of Aerospace Engineering, Vol. 2015, Article ID 781472.
  9. Jacewicz M., Glebocki R., and Ozog R. Monte-Carlo based lateral thruster parameters optimization for 122 mm rocket, In: Conference of Automation, Cham: Springer Nature Switzerland, 2020, pp. 125-134.
  10. Glebocki R., and Jacewicz M. Parametric Study of Guidance of a 160-mm Projectile Steered with Lateral Thrusters, Aerospace, Vol. 7, Iss. 5, May 2020, 61.
  11. Ozog R., Jacewicz M., and Glebocki R. Modified trajectory tracking guidance for artillery rocket, Journal of Theoretical and Applied Mechanics, Vol. 58, No. 3, 2020, pp. 611-622.
  12. Jacewicz M., Lichota P., Miedzinski D., and Glebocki R. Study of Model Uncertainties Influence on the Impact Point Dispersion for a Gasodynamicaly Controlled Projectile, Sensors, Vol. 22, Iss. 9, May 2022, 3257.
  13. Miedzinski D., Glebocki R., and Jacewicz M. Analysis of Sounding Rocket Dispersion Using Monte-Carlo Simulation, In: Conference of Automation, Cham: Springer Nature Switzerland, 2023, pp. 39-50.
  14. Machala D., Dobre S., Albisser M., Gilson M., and Collin F. The Analysis of Vehicle’s In-Flight Behaviour Using Quasi-LPV and Nonlinear Models, AIAA Scitech 2019 Forum, San Diego, CA, USA, January 2019.
Language: English
Page range: 94 - 101
Published on: Jul 5, 2025
Published by: Nicolae Balcescu Land Forces Academy
In partnership with: Paradigm Publishing Services
Publication frequency: 3 issues per year

© 2025 Marius-Ionuț Mărmureanu, published by Nicolae Balcescu Land Forces Academy
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.