Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints

阶段(地层学) 领域(数学) 航空航天工程 计算机科学 控制理论(社会学) 工程类 地质学 数学 控制(管理) 人工智能 古生物学 纯数学
作者
Xiao-Yan Yang,Yuchen Zhang,Shenmin Song
出处
期刊:Journal of Guidance Control and Dynamics [American Institute of Aeronautics and Astronautics]
卷期号:46 (3): 590-599 被引量:1
标识
DOI:10.2514/1.g007040
摘要

No AccessEngineering NotesTwo-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View ConstraintsXiaoyan Yang, Yuchen Zhang and Shenmin SongXiaoyan Yang https://orcid.org/0000-0001-5559-7164Harbin Institute of Technology, 150001 Harbin, People’s Republic of China*Ph.D. Student, School of Aeronautics, Heilongjiang; .Search for more papers by this author, Yuchen ZhangHarbin Institute of Technology, 150001 Harbin, People’s Republic of China†Ph.D. Student, School of Aeronautics, Heilongjiang; .Search for more papers by this author and Shenmin SongHarbin Institute of Technology, 150001 Harbin, People’s Republic of China‡Professor, School of Aeronautics, Heilongjiang; (Corresponding Author).Search for more papers by this authorPublished Online:25 Oct 2022https://doi.org/10.2514/1.G007040SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Lee J., Jeon I. and Tahk M., “Guidance Law to Control Impact Time and Angle,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 43, No. 1, 2007, pp. 301–310. https://doi.org/10.1109/TAES.2007.357135 CrossrefGoogle Scholar[2] Erer K.-S. and Tekin R., “Impact Time and Angle Control Based on Constrained Optimal Solutions,” Journal of Guidance, Control, and Dynamics, Vol. 39, No. 10, 2016, pp. 2448–2454. https://doi.org/10.2514/1.G000414 LinkGoogle Scholar[3] Livermore R. and Shima T., “Deviated Pure-Pursuit-Based Optimal Guidance Law for Imposing Intercept Time and Angle,” Journal of Guidance, Control, and Dynamics, Vol. 41, No. 8, 2018, pp. 1807–1814. https://doi.org/10.2514/1.G003179 LinkGoogle Scholar[4] Chen X. and Wang J., “Optimal Control-Based Guidance Law to Control Both Impact Time and Impact Angle,” Aerospace Science and Technology, Vol. 84, 2019, pp. 454–463. https://doi.org/10.1016/j.ast.2018.10.036 CrossrefGoogle Scholar[5] Zhang Y., Ma G. and Liu A., “Guidance Law with Impact Time and Impact Angle Constraints,” Chinese Journal of Aeronautics, Vol. 26, No. 4, 2013, pp. 960–966. https://doi.org/10.1016/j.cja.2013.04.037 CrossrefGoogle Scholar[6] Zhu J., Su D., Xie Y. and Sun H., “Impact Time and Angle Control Guidance Independent of Time-to-Go Prediction,” Aerospace Science and Technology, Vol. 86, March 2019, pp. 818–825. https://doi.org/10.1016/j.ast.2019.01.047 CrossrefGoogle Scholar[7] Harl N. and Balakrishnan S.-N., “Impact Time and Angle Guidance with Sliding Mode Control,” IEEE Transactions on Control Systems Technology, Vol. 20, No. 6, 2012, pp. 1436–1449. https://doi.org/10.1109/TCST.2011.2169795 CrossrefGoogle Scholar[8] Zhao Y., Sheng Y. and Liu X., “Analytical Impact Time and Angle Guidance via Time-Varying Sliding Mode Technique,” ISA Transactions, Vol. 62, May 2016, pp. 164–176. https://doi.org/10.1016/j.isatra.2016.02.002 CrossrefGoogle Scholar[9] Chen X. and Wang J., “Sliding-Mode Guidance for Simultaneous Control of Impact Time and Angle,” Journal of Guidance, Control, and Dynamics, Vol. 42, No. 2, 2019, pp. 394–401. https://doi.org/10.2514/1.G003893 LinkGoogle Scholar[10] Hou Z., Yang Y., Liu L. and Wang Y., “Terminal Sliding Mode Control-Based Impact Time and Angle Constrained Guidance,” Aerospace Science and Technology, Vol. 93, Oct. 2019, Paper 105142. https://doi.org/10.1016/j.ast.2019.04.050 Google Scholar[11] Kim T.-H., Lee C.-H., Jeon I.-S. and Tahk M.-J., “Augmented Polynomial Guidance with Impact Time and Angle Constraints,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 49, No. 4, 2013, pp. 2806–2817. https://doi.org/10.1109/TAES.2013.6621856 CrossrefGoogle Scholar[12] Han T., Hu Q. and Xin M., “Analytical Solution of Field-of-View Limited Guidance with Constrained Impact and Capturability Analysis,” Aerospace Science and Technology, Vol. 97, Feb. 2020, Paper 105586. https://doi.org/10.1016/j.ast.2019.105586 Google Scholar[13] Kang S., Tekin R. and Holzapfel F., “Generalized Impact Time and Angle Control via Look-Angle Shaping” Journal of Guidance, Control, and Dynamics, Vol. 42, No. 3, 2019, pp. 695–702. https://doi.org/10.2514/1.G003765 LinkGoogle Scholar[14] Tekin R. and Erer K., “Impact Time and Angle Control Against Moving Targets with Look Angle Shaping,” Journal of Guidance, Control, and Dynamics, Vol. 43, No. 5, 2020, pp. 1020–1025. https://doi.org/10.2514/1.G004762 LinkGoogle Scholar[15] Kim H.-G., Lee J.-Y., Kim H.-J., Kwon H.-H. and Park J.-S., “Look-Angle-Shaping Guidance Law for Impact Angle and Time Control with Field-of-View Constraint,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 56, No. 2, 2020, pp. 1602–1612. https://doi.org/10.1109/TAES.2019.2924175 CrossrefGoogle Scholar[16] Wang P., Guo Y., Ma G., Lee C.-H. and Wie B., “New Look-Angle Tracking Guidance Strategy for Impact Time and Angle Control,” Journal of Guidance, Control, and Dynamics, Vol. 45, No. 3, 2022, pp. 545–557. https://doi.org/10.2514/1.G006229 LinkGoogle Scholar[17] Chen X. and Wang J., “Two-Stage Guidance Law with Impact Time and Angle Constraints,” Nonlinear Dynamics, Vol. 95, No. 3, 2019, pp. 2575–2590. https://doi.org/10.1007/s11071-018-4710-3 CrossrefGoogle Scholar[18] Hu Q., Han T. and Xin M., “New Impact Time and Angle Guidance Strategy via Virtual Target Approach,” Journal of Guidance, Control, and Dynamics, Vol. 41, No. 8, 2018, pp. 1755–1765. https://doi.org/10.2514/1.G003436 LinkGoogle Scholar[19] Wang Z., Hu Q., Han T. and Xin M., “Two-Stage Guidance Law with Constrained Impact via Circle Involute,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 57, No. 2, 2021, pp. 1301–1316. https://doi.org/10.1109/TAES.2020.3040524 CrossrefGoogle Scholar[20] Zhang Z., Ma K., Zhang G. and Yan L., “Virtual Target Approach-Based Optimal Guidance Law with Both Impact Time and Terminal Angle Constraints,” Nonlinear Dynamics, Vol. 107, No. 4, 2022, pp. 3521–3541. https://doi.org/10.1007/s11071-021-07142-3 CrossrefGoogle Scholar[21] Zhang S., Guo Y., Liu Z., Wang S. and Hu X., “Finite-Time Cooperative Guidance Strategy for Impact Angle and Time Control,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 57, No. 2, 2021, pp. 806–819. https://doi.org/10.1109/TAES.2020.3037958 CrossrefGoogle Scholar[22] Chen Z., Chen W., Liu X. and Cheng J., “Three-Dimensional Fixed-Time Robust Cooperative Guidance Law for Simultaneous Attack with Impact Angle Constraint,” Aerospace Science and Technology, Vol. 110, March 2021, pp. 1270–9638. https://doi.org/10.1016/j.ast.2021.106523. Google Scholar[23] Wang X., Zhang Y. and Wu H., “Distributed Cooperative Guidance of Multiple Anti-Ship Missiles with Arbitrary Impact Angle Constraint,” Aerospace Science and Technology, Vol. 46, Oct. 2015, pp. 299–311. https://doi.org/10.1016/j.ast.2015.08.002 CrossrefGoogle Scholar[24] Wang C., Wang J. and Xin M., “Impact-Angle-Constrained Cooperative Guidance for Salvo Attack,” Journal of Guidance, Control, and Dynamics, Vol. 45, No. 4, 2022, pp. 684–703. https://doi.org/10.2514/1.G006342 LinkGoogle Scholar[25] Chen Y., Wang J., Wang C., Shan J. and Xin M., “Three-Dimensional Cooperative Homing Guidance Law with Field-of-View Constraint,” Journal of Guidance, Control, and Dynamics, Vol. 43, No. 2, 2020, pp. 389–397. https://doi.org/10.2514/1.G004681 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 46, Number 3March 2023 CrossmarkInformationCopyright © 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsControl TheoryGuidance, Navigation, and Control SystemsHoming GuidanceMissile Guidance and ControlMissile Systems, Dynamics and Technology KeywordsGuidance, Navigation, and Control SystemsSliding Mode ControlHoming GuidanceAcknowledgmentsThis work was supported by the Aeronautical Science Foundation of China (grant numbers 20170112012, 20180112003).PDF Received4 June 2022Accepted13 September 2022Published online25 October 2022

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