Pilóta nélküli légi járművek rajirányítási és rakétavezérlési vizsgálata komplex légi műveletek során
Copyright (c) 2026 Papp István, Békési Bertold, Károly Krisztián

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
Absztrakt
A pilóta nélküli légi járműveket (UAV) egyre szélesebb körben alkalmazzák mind a katonai, mind pedig a polgári szférában. Az orosz–ukrán háború bebizonyította ezen eszközök létjogosultságát, különösen a rakétahordozó jellegű támadásokban, és kulcsszerepet fognak betölteni a jövőbeni háborúkban mint különleges harci mód. A szerzők összegzik a rakétahordozó támadási művelet irányítási és vezérlési eljárásait, bemutatják az irányító- és vezérlőrendszer hagyományos tervezési megoldásait, ezt követően pedig elemzik a jellegzetes rajtámadás irányítási és vezérlési módszereit a megfelelő jellemzők figyelembevételével, és kitérnek a hagyományos tervezési módszerek korlátjaira. A cikk az intelligens integrált irányítási és vezérlési tervezés előnyeire koncentrál a hagyományos tervezési ötletekkel szemben. Összegzi az általánosan alkalmazott integrált irányítási és vezérléstervezési módszereket és azok felhasználásait, valamint feltárja az integrált irányító- és vezérlőrendszerhez megfelelő rakétahordozó kooperatív támadási stratégiáját. Megvizsgálja a rakétahordozók irányításának és vezérlésének kihívásait, és feltárja azokat a problémákat, amelyek a jövőben további kutatásra érdemesek. A rakéták irányítási és vezérlési módszereinek összefoglalása hozzájárul az innovatív kutatáshoz ezen a területen, ami elősegíti a pilóta nélküli rajtámadási technológia fejlődését.
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Hivatkozások
MALIK, Zishan et al. (2021): Cooperative Guidance Scheme for Flight of Multiple Combat Uavs Against a Non-Accelerating Moving Target. Proceedings of the 2021 International Bhurban Conference On Applied Sciences And Technologies (IBCAST). Islamabad. Online: https://doi.org/10.1109/ibcast51254.2021.9393309
SHIN, Heemin (2018): An Autonomous Aerial Combat Framework for Two-On-Two Engagements Based on Basic Fighter Maneuvers. Aerospace Science and Technology, 72, 305–315. Online: https://doi.org/10.1016/j.ast.2017.11.014
HANQIAO, Huang et al. (2022): Intelligent Guidance and Control Methods for Missile Swarm. Computational Intelligence and Neuroscience, Wiley Online Library. Online: https://doi.org/10.1155/2022/8235148
ZHANG, Qirui – WEI, Ruixuan (2019): Ground Attack Strategy of Cooperative UAVs for Multitargets. Complexity, 9428087. Online: https://doi.org/10.1155/2019/9428087
DANIAL, Syed Nasir et al. (2019): Situation Awareness Modeling for Emergency Management on Offshore Platforms. Human-centric Computing and Inswarm Sciences, 9(37), 1–26. Online: https://doi.org/10.1186/s13673-019-0199-0
NOBAHARI, Hadi – NASROLLAHI, Saeed (2020): A Nonlinear Robust Model Predictive Differential Game Guidance Algorithm Based on the Particle Swarm Optimization. Journal of the Franklin Institute, 357(15), 11042–11071. Online: https://doi.org/10.1016/j.jfranklin.2020.08.032
ZHOU, Kai et al. (2020): An Air Combat Decision Learning System Based on a Brain-Like Cognitive Mechanism. Cognitive Computation, 12(4), 128–139. Online: https://doi.org/10.1007/s12559-019-09683-7
KUCHAR, James K. – YANG, Lee C. (2000): A Review of Conflict Detection and Resolution Modeling Methods. IEEE Transactions on Intelligent Transportation Systems, 1(4), 179–189. Online: https://doi.org/10.1109/6979.898217
YU, Wenwu et al. (2013): Distributed Control Gains Design for Consensus in Multi-Agent Systems with Second-Order Nonlinear Dynamics. Automatica, 49(7), 2107–2115. Online: https://doi.org/10.1016/j.automatica.2013.03.005
ZHU, Weiren – DUAN, Haibin (2013): Chaotic Predator-Prey Biogeography-Based Optimization Approach for UAV Path Planning. Aerospace Science and Technology, 32(1), 153–161. Online: https://doi.org/10.1016/J.AST.2013.11.003
LEVY, Maital – SHIMA, Tal – GUTMAN, Shaul (2013): Linear Quadratic Integrated versus Separated Autopilot-Guidance Design. Journal of Guidance, Control, and Dynamics, 36(6), 1722–1730. Online: https://doi.org/10.2514/1.61363
YUEH, William R. – LIN, Ching F. (1984): Optimal Controller for Homing Missile. Proceedings of the American Control Conference, San Diego, CA, USA, 737–742. Online: https://doi.org/10.23919/ACC.1984.4788473
YANG, Biao et al. (2013): Self-Adaptive PID Controller of Microwave Drying Rotary Device Tuning On-Line by Genetic Algorithms. Journal of Central South University, 20, 2685–2692. Online: https://doi.org/10.1007/s11771-013-1784-4
ZHANG, Yu – CHEN, Jing – SHEN, Lincheng (2013): Real-Time Trajectory Planning for UAV Air-To-Surface Attack Using Inverse Dynamics Optimization Method and Receding Horizon Control. Chinese Journal of Aeronautics, 26(4), 1038–1056. Online: https://doi.org/10.1016/j.cja.2013.04.040
GU, Wenjin – ZHAO, Hongchao – ZHANG, Ruchuan (2008): A Three-Dimensional Proportional Guidance Law Based on RBF Neural Network. Proceedings of the 7th World Congress on Intelligent Control And Automation, Chongqing, China, 6978–6982. Online: https://doi.org/10.1109/wcica.2008.4593997
MORGAN, Robert Wes – THARP, Hal – VINCENT, Thomas L. (2011): Minimum Energy Guidance for Aerodynamically Controlled Missiles. IEEE Transactions on Automatic Control, 56(9), 2026–2037. Online: https://doi.org/10.1109/tac.2011.2108619
ZHANYUAN, JIANG et al. (2021): A Modified Proportional Navigation Guidance Law for Impact Time Control. Proceedings of the 2021 6th International Conference on Automation, Control and Robotics Engineering (CACRE), Dalian, China. Online: https://doi.org/10.1109/cacre52464.2021.9501293
LI, Rui – MA, Hongzhong (2020): Research on UAV Swarm Cooperative Reconnaissance and Combat Technology. Proceedings of the 2020 3rd International Conference on Unmanned Systems (ICUS), Harbin, China, 996–999. Online: https://doi.org/10.1109/icus50048.2020.9274902
HOU, Mingzhe – LIANG, Xiaoling – DUAN, Guangren (2013): Adaptive Block Dynamic Surface Control for Integrated Missile Guidance and Autopilot. Chinese Journal of Aeronautics, 26(3), 741–750. Online: https://doi.org/10.1016/j.cja.2013.04.035
FU, Zhenhua et al. (2020): Integrated Guidance and Control with Input Saturation and Impact Angle Constraint. Discrete Dynamics in Nature and Society, 5917983. Online: https://doi.org/10.1155/2020/5917983
WILLIAMS, Douglas – RICHMAN, Jack – FRIEDLAND, Bernard (1983): Design of an Integrated Strapdown Guidance and Control System for a Tactical Missile. Proceedings of Guidance and Control Conference, Gatlinburg, TN, USA, 57–66. Online: https://doi.org/10.2514/6.1983-2169
LIN, Ching Fang et al. (1998): Optimal Design of Integrated Missile Guidance and Control. Proceedings of the World Aviation Conference, 1–13. Online: https://doi.org/10.2514/6.1998-5519
MENON, P. – OHLMEYER, Ernest J. (2001): Nonlinear Integrated Guidance-Control Laws for Homing Missiles. Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, Montreal, Canada, 1–9. Online: https://doi.org/10.2514/6.2001-4160
ZHAO, Jinlong – ZHOU, Jun (2016): Receding Horizon Integrated Guidance and Control for Interceptors Based on Gauss Pseudospectral Method. Proceedings of the 2016 IEEE Chinese Guidance, Navigation and Control Conference, Nanjing, China, 1270–1275. Online: https://doi.org/10.1109/CGNCC.2016.7828971
SHARMA, Manu – RICHARDS, Nathan (2004): Adaptive Integrated Guidance and Control for Missile Interceptors. Proceedings of AIAA Guidance, Navigation, and Control Conference, Rhode Island, 1–15. Online: https://doi.org/10.2514/6.2004-4880
SHIMA, Tal – IDAN, Moshe – GOLAN, Oded M. (2006): Sliding-Mode Control for Integrated Missile Autopilot-Guidance. Journal of Guidance, Control, and Dynamics, 29(2), 250–260. Online: https://doi.org/10.2514/1.14951
HUO, Ran et al. (2017): Integrated Guidance and Control Based On High-Order Sliding Mode Method. Proceedings Of the 36th Chinese Control Conference, Dalian, China, 6073–6078. Online: https://doi.org/10.23919/chicc.2017.8028323
HONG, Toan Dinh et al. (2017): Active Disturbance Rejection Control Design for Integrated Guidance and Control Missile Based SMC and Extended State Observer. Proceedings of the 2017 International Conference on System Science and Engineering, Ho Chi Minh City, Vietnam, 476–481. Online: https://doi.org/10.1109/ICSSE.2017.8030920
JIAN, Chen et al. (2016): Integrated Guidance and Control Design Based on a Reference Model. International Journal of Control, Automation and Systems, 14(5), 1299–1308. Online: https://doi.org/10.1007/s12555-015-0048-5
ZHU, Guodong – SHEN, Zuojun (2015): Three Dimensional Trajectory Linearization Control for Flight of Air-Breathing Hypersonic Vehicle. Procedia Engineering, 99, 1108–1119. Online: https://doi.org/10.1016/j.proeng.2014.12.646
ZHOU, Huan et al. (2015): Robust Integrated Guidance and Control Design Method for UAV Based on Trajectory Linearization Control. Proceedings of the 15th International Conference on Control, Automation and Systems, Busan, Korea (South). Online: https://doi.org/10.1109/ICCAS.2015.7364797
ZHANG, Xue et al. (2020): Nonlinear Distributed Model Predictive Control for Multiple Missiles Against Maneuvering Target with a Trajectory Predictor. Journal of Shanghai Jiaotong University, 25, 779–789. Online: https://doi.org/10.1007/s12204-020-2233-9