Trajectory prediction-based guidance law
This paper proposes a guidance law based on trajectory prediction, aiming to address the difficulty of traditional guidance laws in meeting high-speed and highly maneuverable vehicles. The unscented Kalman filtering (UKF) technique is employed to estimate the target’s motion and predict the virtual...
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| Vydáno v: | Journal of physics. Conference series Ročník 2691; číslo 1; s. 12034 - 12041 |
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| Hlavní autoři: | , , |
| Médium: | Journal Article |
| Jazyk: | angličtina |
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Bristol
IOP Publishing
01.01.2024
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| ISSN: | 1742-6588, 1742-6596 |
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| Abstract | This paper proposes a guidance law based on trajectory prediction, aiming to address the difficulty of traditional guidance laws in meeting high-speed and highly maneuverable vehicles. The unscented Kalman filtering (UKF) technique is employed to estimate the target’s motion and predict the virtual impact point using the Singer model and measuring model. The midcourse guidance law is applied to the virtual target, taking into account the constraint of the intersection angle, while the terminal guidance utilizes modified proportional guidance. To mitigate the overload chattering in the transition sections of both midcourse and terminal guidance, the distance is used to modify the transition section of the terminal guidance. Simulation results demonstrate that the proposed guidance law effectively reduces both the encounter angle and the required maneuvering. Furthermore, to minimize midcourse guidance errors, the prediction results of the virtual target are continually updated during the trace process. This method can also be applied to trail other highly maneuverable targets. |
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| AbstractList | This paper proposes a guidance law based on trajectory prediction, aiming to address the difficulty of traditional guidance laws in meeting high-speed and highly maneuverable vehicles. The unscented Kalman filtering (UKF) technique is employed to estimate the target’s motion and predict the virtual impact point using the Singer model and measuring model. The midcourse guidance law is applied to the virtual target, taking into account the constraint of the intersection angle, while the terminal guidance utilizes modified proportional guidance. To mitigate the overload chattering in the transition sections of both midcourse and terminal guidance, the distance is used to modify the transition section of the terminal guidance. Simulation results demonstrate that the proposed guidance law effectively reduces both the encounter angle and the required maneuvering. Furthermore, to minimize midcourse guidance errors, the prediction results of the virtual target are continually updated during the trace process. This method can also be applied to trail other highly maneuverable targets. |
| Author | Li, Mengxuan Jiang, Ruimin Guo, Jianguo |
| Author_xml | – sequence: 1 givenname: Mengxuan surname: Li fullname: Li, Mengxuan organization: Institute of Precision Guidance and Control, Northwestern Polytechnical University , China – sequence: 2 givenname: Jianguo surname: Guo fullname: Guo, Jianguo organization: Institute of Precision Guidance and Control, Northwestern Polytechnical University , China – sequence: 3 givenname: Ruimin surname: Jiang fullname: Jiang, Ruimin organization: Institute of Precision Guidance and Control, Northwestern Polytechnical University , China |
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| Cites_doi | 10.1007/s12555-010-0213-9 10.1016/j.isatra.2012.11.005 10.2514/1.51543 |
| ContentType | Journal Article |
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| DOI | 10.1088/1742-6596/2691/1/012034 |
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| References | Shiguo (JPCS_2691_1_012034bib11) 2011 Zhai (JPCS_2691_1_012034bib2) 2016; 37 Dwivedi (JPCS_2691_1_012034bib4) 2013 Wang (JPCS_2691_1_012034bib3) 2021; 49 Yamasaki (JPCS_2691_1_012034bib7) 2013 Liang (JPCS_2691_1_012034bib8) 2013 Hexner (JPCS_2691_1_012034bib10) 2011; 34 Evcimen (JPCS_2691_1_012034bib6) 2013 Chen (JPCS_2691_1_012034bib5) 2010; 8 Shafiei (JPCS_2691_1_012034bib9) 2013; 52 Qin (JPCS_2691_1_012034bib1) 2015; 33 |
| References_xml | – volume: 8 start-page: 272 year: 2010 ident: JPCS_2691_1_012034bib5 article-title: Design of midcourse guidance laws via a combination of fuzzy and SMC approaches publication-title: J. International Journal of Control, Automation and Systems doi: 10.1007/s12555-010-0213-9 – start-page: 4784 year: 2013 ident: JPCS_2691_1_012034bib6 article-title: An adaptive, optimal proportional-integral guidance for missiles – volume: 52 start-page: 192 year: 2013 ident: JPCS_2691_1_012034bib9 article-title: Application of partial sliding mode in guidance problem publication-title: J. ISA transactions doi: 10.1016/j.isatra.2012.11.005 – start-page: 478 year: 2011 ident: JPCS_2691_1_012034bib11 article-title: A new optimal guidance law for Near Space Hypersonic Vehicle based on Markov jump linear system – volume: 33 start-page: 56 year: 2015 ident: JPCS_2691_1_012034bib1 article-title: The Problems of Tracking Filter and Prediction for Non-ballistic Target HTV-2 in the Near Space publication-title: J. Aerospace Control – volume: 37 start-page: 3466 year: 2016 ident: JPCS_2691_1_012034bib2 article-title: Trajectory prediction of hypersonic vehicle based on adaptive IMM publication-title: J. Acta Aeronautica et Astronautica Sinica – start-page: 5115 year: 2013 ident: JPCS_2691_1_012034bib7 article-title: Second order sliding mode-based intercept guidance with uncertainty and disturbance compensation – start-page: 63 year: 2013 ident: JPCS_2691_1_012034bib8 article-title: A guidance law design using the combination of ISMC and SDRE schemes – volume: 34 start-page: 437 year: 2011 ident: JPCS_2691_1_012034bib10 article-title: Practical stochastic optimal guidance law for bounded acceleration missiles publication-title: J. Journal of guidance, control, and dynamics doi: 10.2514/1.51543 – volume: 49 start-page: 22 year: 2021 ident: JPCS_2691_1_012034bib3 article-title: Development of Near Space Hypersonic Vehicles and Defence Strategies Analysis publication-title: J. Modern Defence Technology – start-page: 4786 year: 2013 ident: JPCS_2691_1_012034bib4 article-title: Lead angle constrained optimal midcourse guidance |
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| SubjectTerms | Kalman filters Maneuverability Midcourse guidance Terminal guidance Trajectories |
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| Title | Trajectory prediction-based guidance law |
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