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Study for a 122 mm Artillery Rocket Steered with Lateral Thrusters

  
05 lip 2025

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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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

Pavkovic B. Research of Projectile Trajectory Correction Methods in Function of Their Range and Precision Enhancement, PhD thesis, University of Belgrade, Serbia, 2012. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar

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. Search in Google Scholar