CLC number:
On-line Access: 2023-04-25
Received: 2022-09-01
Revision Accepted: 2022-12-29
Crosschecked: 2023-04-25
Cited: 0
Clicked: 1417
Citations: Bibtex RefMan EndNote GB/T7714
Shuangxi LIU, Binbin YAN, Wei HUANG, Xu ZHANG, Jie YAN. Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review[J]. Journal of Zhejiang University Science A, 2023, 24(1): 387-403. @article{title="Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review", %0 Journal Article TY - JOUR
拦截临近空间高超声速飞行器末制导律研究进展与展望机构:1西北工业大学,无人系统技术研究院,中国西安,710072;2西北工业大学,航天学院,中国西安,710072;3国防科技大学,空天科学学院,中国长沙,410073 概要:临近空间高超声速飞行器是指在临近空间能够以大于5马赫速度飞行的一类飞行器,具有飞行速度快、突防能力强、作战半径大和响应迅速等特点。凭借其优异的性能优势,高超声速飞行器逐渐成为各个国家新的空天博弈焦点,给现有防御体系带来巨大挑战。为满足临近空间高超声速飞行器防御需求,本文系统性地梳理高超声速飞行器的"五大优势"及拦截高超声速飞行器的"四大难点"。其次,针对现阶段高超声速飞行器拦截制导律,对基于单弹制导律和多弹协同制导律进行综述,并归纳其优缺点。最后,从"信息域"、"空间域"、"物理域"和"效费比"四个方面对协同拦截高超声速飞行器未来发展方向进行了展望,为临近空间拦截制导技术研究提供参考。 关键词组: Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article
Reference[1]ActonJM, 2015. Hypersonic boost-glide weapons. Science & Global Security, 23(3):191-219. ![]() [2]AiXL, WangLL, YuJQ, et al., 2019. Field-of-view constrained two-stage guidance law design for three-dimensional salvo attack of multiple missiles via an optimal control approach. Aerospace Science and Technology, 85:334-346. ![]() [3]AnK, GuoZY, HuangW, et al., 2022a. A cooperative guidance approach based on the finite-time control theory for hypersonic vehicles. International Journal of Aeronautical and Space Sciences, 23(1):169-179. ![]() [4]AnK, GuoZY, HuangW, et al., 2022b. Leap trajectory tracking control based on sliding mode theory for hypersonic gliding vehicle. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 23(3):188-207. ![]() [5]BanasikM, 2021. Global challenges and threats of hypersonic weapons: the Russian context. Safety & Defense, 7(2):40-50. ![]() [6]BianZ, LiJT, GuoLX, 2020. Simulation and feature extraction of the dynamic electromagnetic scattering of a hypersonic vehicle covered with plasma sheath. Remote Sensing, 12(17):2740. ![]() [7]BianZ, LiJT, GuoLX, et al., 2021. Analyzing the electromagnetic scattering characteristics of a hypersonic vehicle based on the inhomogeneity zonal medium model. IEEE Transactions on Antennas and Propagation, 69(2):971-982. ![]() [8]BolenderMA, DomanDB, 2007. Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle. Journal of Spacecraft and Rockets, 44(2):374-387. ![]() [9]BorrieJ, DowlerA, PodvigP, 2019. Hypersonic Weapons: a Challenge and Opportunity for Strategic Arms Control. United Nations Office for Disarmament Affairs, United Nations Institute for Disarmament Research, New York, USA. ![]() [10]ChalangaA, KamalS, FridmanLM, et al., 2016. Implementation of super-twisting control: super-twisting and higher order sliding-mode observer-based approaches. IEEE Transactions on Industrial Electronics, 63(6):3677-3685. ![]() [11]ChenF, HeGJ, HeQF, 2019. A finite-time-convergent composite guidance law with strong fault-tolerant performance. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 233(9):3120-3130. ![]() [12]ChenK, LiangWC, ZengCZ, et al., 2021. Multi-geomagnetic-component assisted localization algorithm for hypersonic vehicles. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 22(5):357-368. ![]() [13]ChenK, ZengCZ, PeiSS, et al., 2022. Normal gravity model for inertial navigation of a hypersonic boost-glide vehicle. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 23(10):55-67. ![]() [14]ChenXT, WangJZ, 2019. Optimal control based guidance law to control both impact time and impact angle. Aerospace Science and Technology, 84:454-463. ![]() [15]ChenYD, WangJA, ShanJY, et al., 2021. Cooperative guidance for multiple powered missiles with constrained impact and bounded speed. Journal of Guidance, Control, and Dynamics, 44(4):825-841. ![]() [16]ChengL, WangZB, JiangFH, et al., 2021. Adaptive neural network control of nonlinear systems with unknown dynamics. Advances in Space Research, 67(3):1114-1123. ![]() [17]CottrellRG, VincentTL, SadatiSH, 1996. Minimizing interceptor size using neural networks for terminal guidance law synthesis. Journal of Guidance, Control, and Dynamics, 19(3):557-562. ![]() [18]DavisS, 2020. Hypersonic Weapons–a Technological Challenge for Allied Nations and NATO? NATO Parliamentary Assembly. ![]() [19]DimirovskiGM, DeskovskiSM, GacovskiZM, 2004. Classical and fuzzy-system guidance laws in homing missiles systems. 2004 IEEE Aerospace Conference Proceedings, p.3032-3047. ![]() [20]DingYB, YueXK, ChenGS, et al., 2022. Review of control and guidance technology on hypersonic vehicle. Chinese Journal of Aeronautics, 35(7):1-18. ![]() [21]DongWQ, HeF, 2021. Hierarchical and distributed generation of information interaction topology for large scale UAV formation. Acta Aeronautica et Astronautica Sinica, 42(6):324380 (in Chinese). ![]() [22]DrakesJA, HiersIII RS, ReedRA, 1992. Doppler shift effects on infrared band models. Journal of Thermophysics and Heat Transfer, 6(1):44-47. ![]() [23]DumitrescuC, CiotirnaeP, VizitiuC, 2021. Fuzzy logic for intelligent control system using soft computing applications. Sensors, 21(8):2617. ![]() [24]EkmektsioglouE, 2015. Hypersonic weapons and escalation control in East Asia. Strategic Studies Quarterly, 9(2):43-68. ![]() [25]ElhalwagyYZ, TarbouchiM, 2004. Fuzzy logic sliding mode control for command guidance law design. ISA Transactions, 43(2):231-242. ![]() [26]FangF, CaiYL, JabbariF, 2019. 3D optimal defensive guidance strategy with safe distance. Transactions of the Institute of Measurement and Control, 41(15):4285-4300. ![]() [27]FedericiL, BenedikterB, ZavoliA, 2021. Deep learning techniques for autonomous spacecraft guidance during proximity operations. Journal of Spacecraft and Rockets, 58(6):1774-1785. ![]() [28]FuQ, FanCL, WangG, et al., 2017. Research on multi-sensor cooperative tracking mission planning of aerospace hypersonic vehicles. The 2nd International Conference on Control, Automation and Artificial Intelligence, p.201-206. ![]() [29]GengZJ, McCulloughCL, 1997. Missile control using fuzzy cerebellar model arithmetic computer neural networks. Journal of Guidance, Control, and Dynamics, 20(3):557-565. ![]() [30]GengZJ, XuR, McCulloughCL, 1995. Missile control using the fuzzy CMAC neural networks. Guidance, Navigation, and Control Conference, p.901. ![]() [31]GuWJ, ZhaoHC, ZhangRC, 2008. A three-dimensional proportional guidance law based on RBF neural network. The 7th World Congress on Intelligent Control and Automation, p.6978-6982. ![]() [32]GubrudM, 2015. Going too fast: time to ban hypersonic missile tests? A US response. Bulletin of the Atomic Scientists, 71(5):1-4. ![]() [33]GuoY, YaoY, WangSC, et al., 2013. Maneuver control strategies to maximize prediction errors in ballistic middle phase. Journal of Guidance, Control, and Dynamics, 36(4):1225-1234. ![]() [34]GutmanS, 1979. On optimal guidance for homing missiles. Journal of Guidance and Control, 2(4):296-300. ![]() [35]HanT, HuQL, ShinHS, et al., 2021. Sensor-based robust incremental three-dimensional guidance law with terminal angle constraint. Journal of Guidance, Control, and Dynamics, 44(11):2016-2030. ![]() [36]HanT, ShinHS, HuQL, et al., 2022a. Differentiator-based incremental three-dimensional terminal angle guidance with enhanced robustness. IEEE Transactions on Aerospace and Electronic Systems, 58(5):4020-4032. ![]() [37]HanT, HuQL, XinM, 2022b. Three-dimensional approach angle guidance under varying velocity and field-of-view limit without using line-of-sight rate. IEEE Transactions on Systems, Man, and Cybernetics: Systems, 52(11):7148-7159. ![]() [38]HassanL, SadatiSH, KarimiJ, 2013. Integrated fuzzy guidance law for high maneuvering targets based on proportional navigation guidance. Iranian Journal of Electrical & Electronic Engineering, 9(4):204-214. ![]() [39]HuQL, HanT, XinM, 2018. New impact time and angle guidance strategy via virtual target approach. Journal of Guidance, Control, and Dynamics, 41(8):1755-1765. ![]() [40]HuYD, GaoCS, LiJL, et al., 2021. Novel trajectory prediction algorithms for hypersonic gliding vehicles based on maneuver mode on-line identification and intent inference. Measurement Science and Technology, 32(11):115012. ![]() [41]HuaWH, ChenXL, 2011. Nonlinear bounded-control differential game guidance law for variable-speed missiles. Control and Decision, 26(12):1886-1890 (in Chinese). ![]() [42]HuaWH, LiuY, ChenXL, et al., 2011. Linear quadratic differential game guidance law with terminal constraints. Acta Armamentarii, 32(12):1448-1455 (in Chinese). ![]() [43]HuaWH, MengQL, ZhangJP, et al., 2016. Differential game guidance law for dual and bounded controlled missiles. Journal of Beijing University of Aeronautics and Astronautics, 42(9):1851-1856 (in Chinese). ![]() [44]HuiYL, NanY, ChenSD, et al., 2015. Research on cooperative multiple-missile intercepting strategy for near-space vehicles. Journal of Projectiles, Rockets, Missiles and Guidance, 35(5):149-154 (in Chinese). ![]() [45]IzzoD, ÖztürkE, 2021. Real-time guidance for low-thrust transfers using deep neural networks. Journal of Guidance, Control, and Dynamics, 44(2):315-327. ![]() [46]KumarA, OjhaA, PadhyPK, 2017. Anticipated trajectory based proportional navigation guidance scheme for intercepting high maneuvering targets. International Journal of Control, Automation and Systems, 15(3):1351-1361. ![]() [47]LawsonRA, McDermottLC, 1987. Student understanding of the work-energy and impulse-momentum theorems. American Journal of Physics, 55(9):811-817. ![]() [48]LiKB, LiangYG, SuWS, et al., 2018. Performance of 3D TPN against true-arbitrarily maneuvering target for exoatmospheric interception. Science China Technological Sciences, 61(8):1161-1174. ![]() [49]LiQC, ZhangWS, HanG, et al., 2015. Finite time convergent wavelet neural network sliding mode control guidance law with impact angle constraint. International Journal of Automation and Computing, 12(6):588-599. ![]() [50]LiQC, ZhangWS, HanG, et al., 2016. Fuzzy sliding mode control guidance law with terminal impact angle and acceleration constraints. Journal of Systems Engineering and Electronics, 27(3):664-679. ![]() [51]LiWH, MengYS, 2020. Missile weapon system boost the development of war. Tactical Missile Technology, (4):161-166 (in Chinese). ![]() [52]LiZJ, XiaYQ, SuCY, et al., 2015. Missile guidance law based on robust model predictive control using neural-network optimization. IEEE Transactions on Neural Networks and Learning Systems, 26(8):1803-1809. ![]() [53]LinCL, ChenYY, 2000. Design of fuzzy logic guidance law against high-speed target. Journal of Guidance, Control, and Dynamics, 23(1):17-25. ![]() [54]LiuDX, WangJL, XuK, et al., 2019. Task-driven relay assignment in distributed UAV communication networks. IEEE Transactions on Vehicular Technology, 68(11):11003-11017. ![]() [55]LiuSX, YanBB, ZhangT, et al., 2021. Guidance law with desired impact time and FOV constrained for antiship missiles based on equivalent sliding mode control. International Journal of Aerospace Engineering, 2021:9923332. ![]() [56]LiuSX, YanBB, LiuRF, et al., 2022a. Cooperative guidance law for intercepting a hypersonic target with impact angle constraint. The Aeronautical Journal, 126(1300):1026-1044. ![]() [57]LiuSX, YanBB, ZhangT, et al., 2022b. Coverage-based cooperative guidance law for intercepting hypersonic vehicles with overload constraint. Aerospace Science and Technology, 126:107651. ![]() [58]LiuSX, YanBB, ZhangX, et al., 2022c. Fractional-order sliding mode guidance law for intercepting hypersonic vehicles. Aerospace, 9(2):53. ![]() [59]LiuSX, WangYC, ZhuMJ, et al., 2022d. Research on differential game guidance law for intercepting hypersonic vehicles with small missile-to-target speed ratio. Air & Space Defense, 5(2):49-57 (in Chinese). ![]() [60]LiuSX, YanBB, ZhangT, et al., 2022e. Three-dimensional cooperative guidance law for intercepting hypersonic targets. Aerospace Science and Technology, 129:107815. ![]() [61]LiuSX, YanBB, ZhangT, et al., 2022f. Three-dimensional coverage-based cooperative guidance law with overload constraints to intercept a hypersonic vehicle. Aerospace Science and Technology, 130:107908. ![]() [62]LiuYC, ZhuQD, FanX, 2023. Event-triggered adaptive fuzzy control for stochastic nonlinear time-delay systems. Fuzzy Sets and Systems, 452:42-60. ![]() [63]MishraSK, SarmaIG, SwamyKN, 1994. Performance evaluation of two fuzzy-logic-based homing guidance schemes. Journal of Guidance, Control, and Dynamics, 17(6):1389-1391. ![]() [64]MitchellIM, BayenAM, TomlinCJ, 2005. A time-dependent Hamilton-Jacobi formulation of reachable sets for continuous dynamic games. IEEE Transactions on Automatic Control, 50(7):947-957. ![]() [65]NagappaR, 2015. Going too fast: time to ban hypersonic missile tests? An Indian response. Bulletin of the Atomic Scientists, 71(5):9-12. ![]() [66]NielsenJN, 1988. Missile Aerodynamics. American Institute of Aeronautics and Astronautics, Inc., Reston, USA. ![]() [67]OshmanY, RadDA, 2006. Differential-game-based guidance law using target orientation observations. IEEE Transactions on Aerospace and Electronic Systems, 42(1):316-326. ![]() [68]ParkBG, KimTH, TahkMJ, 2013. Optimal impact angle control guidance law considering the seeker’s field-of-view limits. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 227(8):1347-1364. ![]() [69]PastrickHL, SeltzerSM, WarrenME, 1981. Guidance laws for short-range tactical missiles. Journal of Guidance and Control, 4(2):98-108. ![]() [70]RiazU, AminAA, TayyebM, 2022. Design of active fault-tolerant control system for air-fuel ratio control of internal combustion engines using fuzzy logic controller. Science Progress, 105(2):00368504221094723. ![]() [71]SaylerKM, 2019. Hypersonic Weapons: Background and Issues for Congress. Congressional Research Service, USA. https://crsreports.congress.gov/product/pdf/R/R45811/19 ![]() [72]ShiL, ZhuCY, ZhaoL, et al., 2020. Fast Doppler shift acquisition method for hypersonic vehicle communications. IET Communications, 14(3):474-479. ![]() [73]SongJH, SongSM, XuSL, 2017. Three-dimensional cooperative guidance law for multiple missiles with finite-time convergence. Aerospace Science and Technology, 67:193-205. ![]() [74]SunJL, LiuCS, 2017. An overview on the adaptive dynamic programming based missile guidance law. Acta Automatica Sinica, 43(7):1101-1113 (in Chinese). ![]() [75]SunJL, LiuCS, 2019. Distributed fuzzy adaptive backstepping optimal control for nonlinear multimissile guidance systems with input saturation. IEEE Transactions on Fuzzy Systems, 27(3):447-461. ![]() [76]SziroczakD, SmithH, 2016. A review of design issues specific to hypersonic flight vehicles. Progress in Aerospace Sciences, 84:1-28. ![]() [77]TanSL, LeiHM, WangB, 2019. Cooperative guidance law for hypersonic targets with constrained impact angle. Transactions of Beijing Institute of Technology, 39(6):597-602 (in Chinese). ![]() [78]TangJW, HuangZW, ZhuYD, et al., 2022. Neural network compensation control of magnetic levitation ball position based on fuzzy inference. Scientific Reports, 12(1):1795. ![]() [79]WaldmannJ, 2002. Line-of-sight rate estimation and linearizing control of an imaging seeker in a tactical missile guided by proportional navigation. IEEE Transactions on Control Systems Technology, 10(4):556-567. ![]() [80]WangL, LiuK, YaoY, et al., 2022. A design approach for simultaneous cooperative interception based on area coverage optimization. Drones, 6(7):156. ![]() [81]WangYL, TangSJ, ShangW, et al., 2018. Adaptive fuzzy sliding mode guidance law considering available acceleration and autopilot dynamics. International Journal of Aerospace Engineering, 2018:6081801. ![]() [82]WeiXQ, YangJY, FanXR, 2021. Variational method-based distributed optimal guidance laws for multi-attackers’ simultaneous attack. Transactions of the Institute of Measurement and Control, 43(9):1868-1879. ![]() [83]WeissM, ShimaT, 2019. Linear quadratic optimal control-based missile guidance law with obstacle avoidance. IEEE Transactions on Aerospace and Electronic Systems, 55(1):205-214. ![]() [84]WilkeningD, 2019. Hypersonic weapons and strategic stability. Survival, 61(5):129-148. ![]() [85]WilliamsonJ, WirtzJJ, 2021. Hypersonic or just hype? Assessing the Russian hypersonic weapons program. Comparative Strategy, 40(5):468-481. ![]() [86]WorkRO, GrantG, 2019. Beating the Americans at Their Own Game: an Offset Strategy with Chinese Characteristics. Center for a New American Security, Washington, USA, p.195-260. ![]() [87]WuG, ZhangK, 2021. A novel guidance law for intercepting a highly maneuvering target. International Journal of Aerospace Engineering, 2021:2326323. ![]() [88]WuG, ZhangK, HanZ, 2022. Three-dimensional finite-time guidance law based on sliding mode adaptive RBF neural network against a highly manoeuvering target. The Aeronautical Journal, 126(1301):1124-1143. ![]() [89]XieY, LiuLH, TangGJ, et al., 2011. Weaving maneuver trajectory design for hypersonic glide vehicles. Acta Aeronautica et Astronautica Sinica, 32(12):2174-2181 (in Chinese). ![]() [90]XuB, ShiZK, 2015. An overview on flight dynamics and control approaches for hypersonic vehicles. Science China Information Sciences, 58(7):1-19. ![]() [91]YanBB, DaiP, LiuRF, et al., 2019. Adaptive super-twisting sliding mode control of variable sweep morphing aircraft. Aerospace Science and Technology, 92:198-210. ![]() [92]YangB, JingWX, GaoCS, 2020. Three-dimensional cooperative guidance law for multiple missiles with impact angle constraint. Journal of Systems Engineering and Electronics, 31(6):1286-1296. ![]() [93]YangCD, YangCC, 1996a. Analytical solution of 3D true proportional navigation. IEEE Transactions on Aerospace and Electronic Systems, 32(4):1509-1522. ![]() [94]YangCD, YangCC, 1996b. Analytical solution of three-dimensional realistic true proportional navigation. Journal of Guidance, Control, and Dynamics, 19(3):569-577. ![]() [95]YeJK, LeiHM, LiJ, 2017. Novel fractional order calculus extended PN for maneuvering targets. International Journal of Aerospace Engineering, 2017:5931967. ![]() [96]YouH, ZhaoFJ, 2020. Distributed synergetic guidance law for multiple missiles with angle-of-attack constraint. The Aeronautical Journal, 124(1274):533-548. ![]() [97]ZhangC, 2019. Interpretation of the UN report “hypersonic weapons–a challenge and opportunity for strategic arms control”. Tactical Missile Technology, (3):7-11 (in Chinese). ![]() [98]ZhangJB, XiongJJ, LanXH, et al., 2022. Trajectory prediction of hypersonic glide vehicle based on empirical wavelet transform and attention convolutional long short-term memory network. IEEE Sensors Journal, 22(5):4601-4615. ![]() [99]ZhangKQ, YangSC, 2018. Fast convergent nonsingular terminal sliding mode guidance law with impact angle constraint. The 37th Chinese Control Conference, p.2963-2968. ![]() [100]ZhangTT, YanXT, HuangW, et al., 2021a. Design and analysis of the air-breathing aircraft with the full-body wave-ride performance. Aerospace Science and Technology, 119:107133. ![]() [101]ZhangTT, YanXT, HuangW, et al., 2021b. Multidisciplinary design optimization of a wide speed range vehicle with waveride airframe and RBCC engine. Energy, 235:121386. ![]() [102]ZhangX, YanJ, LiuSX, et al., 2022. Enhancing the take-off performance of hypersonic vehicles using the improved chimp optimisation algorithm. The Aeronautical Journal, in press. ![]() [103]ZhangZH, MaKM, ZhangGP, et al., 2022. Virtual target approach-based optimal guidance law with both impact time and terminal angle constraints. Nonlinear Dynamics, 107(4):3521-3541. ![]() [104]ZhaoBQ, DongXW, LiQD, et al., 2020. A combined guidance law for intercepting hypersonic large maneuvering targets. 2020 Chinese Automation Congress, p.1425-1430. ![]() [105]ZhaoJ, ZhouR, JinXL, 2014. Progress in reentry trajectory planning for hypersonic vehicle. Journal of Systems Engineering and Electronics, 25(4):627-639. ![]() [106]ZhaoJB, YangSX, 2017. Review of multi-missile cooperative guidance. Acta Aeronautica et Astronautica Sinica, 38(1):020256 (in Chinese). ![]() [107]ZhaoQL, ChenJ, DongXW, et al., 2016. Cooperative guidance law for heterogeneous missiles intercepting hypersonic weapon. Acta Aeronautica et Astronautica Sinica, 37(3):936-948 (in Chinese). ![]() [108]ZhaoT, 2015. Going too fast: time to ban hypersonic missile tests? A Chinese response. Bulletin of the Atomic Scientists, 71(5):5-8. ![]() [109]ZhongQ, ZhangB, BaoHM, et al., 2019. Analysis of pressure and flow compound control characteristics of an independent metering hydraulic system based on a two-level fuzzy controller. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 20(3):184-200. ![]() [110]ZhouJ, WangY, ZhaoB, 2016. Impact-time-control guidance law for missile with time-varying velocity. Mathematical Problems in Engineering, 2016:7951923. ![]() [111]ZhuCQ, 2021. Design of finite-time guidance law based on observer and head-pursuit theory. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 235(13):1791-1802. ![]() [112]ZhuCQ, GuoZY, 2019. Design of head-pursuit guidance law based on backstepping sliding mode control. International Journal of Aerospace Engineering, 2019:8214042. ![]() [113]ZhuCY, ShiL, LiXP, et al., 2018. Lock threshold deterioration induced by antenna vibration and signal coupling effects in hypersonic vehicle carrier tracking system of Ka band. Chinese Journal of Aeronautics, 31(4):776-781. ![]() Journal of Zhejiang University-SCIENCE, 38 Zheda Road, Hangzhou
310027, China
Tel: +86-571-87952783; E-mail: cjzhang@zju.edu.cn Copyright © 2000 - 2023 Journal of Zhejiang University-SCIENCE |
Open peer comments: Debate/Discuss/Question/Opinion
<1>