Modified trajectory tracking guidance for artillery rocket

Rafał Ożóg , Mariusz Jacewicz , Robert Głębocki

Abstract

This paper contributes to a modified guidance scheme based on a trajectory tracking method which is dedicated for an artillery rocket with a finite set of single use solid propellant side thrusters. Frequency modulation of pulses was used to achieve effective firing logic. The proposed control law is applicable in the last phase of flight when the rocket reaches the vertex of the trajectory. A correction engine activation sequence was chosen in such a way that possibility of rocket axial unbalance is minimized due to motors firing. Numerical simulation results indicate that significant dispersion reduction was achieved and the number of activated side rocket thrusters is minimized. REFERENCES (14) 1. Cao X. B., Xu Y. C., Rui C., Y., Shan Z., Y., 2013, Simulation of trajectory correction for an impulse control mortar projectile with a strapdown laser seeker, Applied Mechanics and Materials, 367, 377-381, DOI: https://doi.org/10.4028/www.sc.... CrossRef 2. Gao M., Zhang Y., Yang S., 2015, Firing control optimization of impulse thrusters for trajectory correction projectiles, International Journal of Aerospace Engineering, 2015, 1-11, DOI: 10.1155/2015/781472. CrossRef 3. Gupta S.K., Saxena S., Singhal A., Ghosh A.K., 2008, Trajectory correction flight control system using pulsejet on an artillery rocket, Defence Science Journal, 58, 1, DOI: 10.14429/dsj.58.1621. CrossRef 4. Jitpraphai T., Burchett B. Costello M., 2001, A comparison of different guidance schemes for a direct fire rocket with a pulse jet control mechanism, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Guidance, Navigation, and Control and Co-located Conferences, DOI: 10.2514/6.2001-4326. CrossRef 5. Jitpraphai T., Costello M., 2001, Dispersion reduction of a direct-fire rocket using lateral pulse jets, Journal of Spacecraft and Rockets, 38, 6, 929-936, DOI: 10.2514/2.3765. CrossRef 6. Mandić S., 2009, Guidance of ground to ground rockets using flight path steering method, Scientific Technical Review, LIX, 3-4, 3-11, UDK: 623.465.3. 7. Mccoy R., 2004, Modern Exterior Ballistics: The Launch and Flight Dynamics of Symmetric Projectiles, Schiffer Publishing, Ltd. 8. Moore F., 1993, State-of-the-art Engineering Aeroprediction Methods with Emphasis on New Semiempirical Techniques for Predicting Nonlinear Aerodynamics on Complete Missile Configurations, Naval Surface Warfare Center, Dahlgren, Virginia. 9. Pavic M., Pavkovic B., Mandic S., Zivkovic S., Cuk D., 2015, Pulse-frequency modulated guidance laws for a mortar missile with a pulse jet control mechanism, The Aeronautical Journal, 119, 1213, 389-405, DOI: 10.1017/S0001924000010526. CrossRef 10. Pavkovic B., 2012a, Enhancing the precision of artillery rockets using pulsejet control systems with active damping, Scientific Technical Review, 62, 2, 10-19, UDK: 621.453/457.001.57:519.637. 11. Pavkovic B., Pavic M., Cuk D., 2012b, Frequency-modulated pulse-jet control of an artillery rocket, Journal of Spacecraft and Rockets, 49, 2, 286-294, DOI: 10.2514/1.A32133. CrossRef 12. Siddiq K.M., Jian C.F., Wen B.Y., 2012, State dependent Riccati equation based roll autopilot for 122mm artillery rocket, International Journal of Aerospace and Mechanical Engineering, 6, 12. 13. Zipfel P., 2014, Modeling and Simulation of Aerospace Vehicle Dynamics, American Institute of Aeronautics and Astronautics, Inc. CrossRef 14. Żugaj M., Głębocki R., 2010, Model of gasodynamic control system for guided bomb, Journal of Theoretical and Applied Mechanics, 48, 1, 27-44. Submit your paper If you submitted your paper before December 20th, 2018 login here Share Send by email Related articles Dual-control missile guidance: a simulation study Indexes Keywords index Topics index Authors index
Author Rafał Ożóg (FPAE / IAAM)
Rafał Ożóg,,
- The Institute of Aeronautics and Applied Mechanics
, Mariusz Jacewicz (FPAE / IAAM)
Mariusz Jacewicz,,
- The Institute of Aeronautics and Applied Mechanics
, Robert Głębocki (FPAE / IAAM)
Robert Głębocki,,
- The Institute of Aeronautics and Applied Mechanics
Journal seriesJournal of Theoretical and Applied Mechanics, ISSN 1429-2955, e-ISSN 2543-6309
Issue year2020
Vol58
No3
Pages611-622
Publication size in sheets0.55
ASJC Classification2600 General Mathematics
Abstract in original languageThis paper contributes to a modified guidance scheme based on a trajectory tracking method which is dedicated for an artillery rocket with a finite set of single use solid propellant side thrusters. Frequency modulation of pulses was used to achieve effective firing logic. The proposed control law is applicable in the last phase of flight when the rocket reaches the vertex of the trajectory. A correction engine activation sequence was chosen in such a way that possibility of rocket axial unbalance is minimized due to motors firing. Numerical simulation results indicate that significant dispersion reduction was achieved and the number of activated side rocket thrusters is minimized. REFERENCES (14) 1. Cao X. B., Xu Y. C., Rui C., Y., Shan Z., Y., 2013, Simulation of trajectory correction for an impulse control mortar projectile with a strapdown laser seeker, Applied Mechanics and Materials, 367, 377-381, DOI: https://doi.org/10.4028/www.sc.... CrossRef 2. Gao M., Zhang Y., Yang S., 2015, Firing control optimization of impulse thrusters for trajectory correction projectiles, International Journal of Aerospace Engineering, 2015, 1-11, DOI: 10.1155/2015/781472. CrossRef 3. Gupta S.K., Saxena S., Singhal A., Ghosh A.K., 2008, Trajectory correction flight control system using pulsejet on an artillery rocket, Defence Science Journal, 58, 1, DOI: 10.14429/dsj.58.1621. CrossRef 4. Jitpraphai T., Burchett B. Costello M., 2001, A comparison of different guidance schemes for a direct fire rocket with a pulse jet control mechanism, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Guidance, Navigation, and Control and Co-located Conferences, DOI: 10.2514/6.2001-4326. CrossRef 5. Jitpraphai T., Costello M., 2001, Dispersion reduction of a direct-fire rocket using lateral pulse jets, Journal of Spacecraft and Rockets, 38, 6, 929-936, DOI: 10.2514/2.3765. CrossRef 6. Mandić S., 2009, Guidance of ground to ground rockets using flight path steering method, Scientific Technical Review, LIX, 3-4, 3-11, UDK: 623.465.3. 7. Mccoy R., 2004, Modern Exterior Ballistics: The Launch and Flight Dynamics of Symmetric Projectiles, Schiffer Publishing, Ltd. 8. Moore F., 1993, State-of-the-art Engineering Aeroprediction Methods with Emphasis on New Semiempirical Techniques for Predicting Nonlinear Aerodynamics on Complete Missile Configurations, Naval Surface Warfare Center, Dahlgren, Virginia. 9. Pavic M., Pavkovic B., Mandic S., Zivkovic S., Cuk D., 2015, Pulse-frequency modulated guidance laws for a mortar missile with a pulse jet control mechanism, The Aeronautical Journal, 119, 1213, 389-405, DOI: 10.1017/S0001924000010526. CrossRef 10. Pavkovic B., 2012a, Enhancing the precision of artillery rockets using pulsejet control systems with active damping, Scientific Technical Review, 62, 2, 10-19, UDK: 621.453/457.001.57:519.637. 11. Pavkovic B., Pavic M., Cuk D., 2012b, Frequency-modulated pulse-jet control of an artillery rocket, Journal of Spacecraft and Rockets, 49, 2, 286-294, DOI: 10.2514/1.A32133. CrossRef 12. Siddiq K.M., Jian C.F., Wen B.Y., 2012, State dependent Riccati equation based roll autopilot for 122mm artillery rocket, International Journal of Aerospace and Mechanical Engineering, 6, 12. 13. Zipfel P., 2014, Modeling and Simulation of Aerospace Vehicle Dynamics, American Institute of Aeronautics and Astronautics, Inc. CrossRef 14. Żugaj M., Głębocki R., 2010, Model of gasodynamic control system for guided bomb, Journal of Theoretical and Applied Mechanics, 48, 1, 27-44. Submit your paper If you submitted your paper before December 20th, 2018 login here Share Send by email Related articles Dual-control missile guidance: a simulation study Indexes Keywords index Topics index Authors index
DOIDOI:10.15632/jtam-pl/121981
URL http://jtam.pl/Modified-trajectory-tracking-guidance-for-artillery-rocket,121981,0,2.html
Languageen angielski
Score (nominal)40
Score sourcejournalList
ScoreMinisterial score = 40.0, 09-09-2020, ArticleFromJournal
Publication indicators WoS Citations = 0; Scopus SNIP (Source Normalised Impact per Paper): 2018 = 0.881; WoS Impact Factor: 2018 = 0.771 (2) - 2018=0.965 (5)
Citation count*
Cite
Share Share

Get link to the record


* presented citation count is obtained through Internet information analysis and it is close to the number calculated by the Publish or Perish system.
Back
Confirmation
Are you sure?