Citation: | DONG Xiwang, YU Jianglong, HUA Yongzhao, et al. Review and prospect of cooperative guidance with attack time consensus for multiple aerial vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1836-1844. doi: 10.13700/j.bh.1001-5965.2022.0368(in Chinese) |
Cooperative guidance issue with attack time consensus is an important branch of cooperative guidance issues. The main research results and classification methods of cooperative guidance with attack time consensus for multiple aerial vehicles are summarized. Firstly, the tactical significance of cooperative guidance with attack time consensus is analyzed. Secondly, two categories of issues are researched depending on how the target moves: cooperative guidance for fixed targets and cooperative guidance for moving or maneuvering targets. Furthermore, a review of the main research results of these two types of cooperative guidance problems is provided.The advantages, disadvantages and scenarios of the above cooperative guidance methods are summarized from the level of research methods. Finally, a summary of the related technical challenges of cooperative guidance with attack time consensus is given, along with a prospective direction for future development.
[1] |
肖增博, 雷虎民, 滕江川, 等. 多导弹协同制导规律研究现状及展望[J]. 航空兵器, 2011(6): 18-22. doi: 10.3969/j.issn.1673-5048.2011.06.006
XIAO Z B, LEI H M, TENG J C, et al. The present status and cooperative prospect of multi-missile guidance law[J]. Aero Weaponry, 2011(6): 18-22(in Chinese). doi: 10.3969/j.issn.1673-5048.2011.06.006
|
[2] |
任章, 于江龙. 多临近空间拦截器编队拦截自主协同制导控制技术研究[J]. 导航定位与授时, 2018, 5(2): 1-6. doi: 10.19306/j.cnki.2095-8110.2018.02.001
REN Z, YU J L. Research on the autonomous cooperative guidance control for the formation interception of multiple near space interceptors[J]. Navigation Positioning and Timing, 2018, 5(2): 1-6(in Chinese). doi: 10.19306/j.cnki.2095-8110.2018.02.001
|
[3] |
ZHAO S Y, ZHOU R. Cooperative guidance for multimissile salvo attack[J]. Chinese Journal of Aeronautics, 2008, 21(6): 533-539. doi: 10.1016/S1000-9361(08)60171-5
|
[4] |
于江龙, 董希旺, 李清东, 等. 拦截机动目标的分布式协同围捕制导方法[J/OL]. 航空学报, 2021(2021-08-17)[2022-05-10]. http://kns.cnki.net/kcms/detail/11.1929.V.20210817.1013.010.html.
YU J L, DONG X W, LI Q D, et al. Distributed cooperative encirclement hunting guidance method for intercepting the maneuvering target[J/OL]. Acta Aeronautica et Astronautica Sinica, 2021(2021-08-17)[2022-05-10]. http://kns.cnki.net/kcms/detail/11.1929.V.20210817.1013.010.html (in Chinese).
|
[5] |
KUMAR S R, SHIMA T. Cooperative nonlinear guidance strategies for aircraft defense[J]. Journal of Guidance, Control, and Dynamics, 2017, 40(1): 124-138. doi: 10.2514/1.G000659
|
[6] |
张帅, 郭杨, 王仕成. 带有引诱角色的有限时间协同制导方法[J]. 宇航学报, 2018, 39(3): 308-317. https://www.cnki.com.cn/Article/CJFDTOTAL-YHXB201803009.htm
ZHANG S, GUO Y, WANG S C. Finite time cooperative guidance method with a lure role[J]. Journal of Astronautics, 2018, 39(3): 308-317(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-YHXB201803009.htm
|
[7] |
王晓芳, 王紫扬, 林海. 一种同时具有攻击时间和攻击角度约束的协同制导律[J]. 弹道学报, 2017, 29(4): 1-8. doi: 10.3969/j.issn.1004-499X.2017.04.001
WANG X F, WANG Z Y, LIN H. A cooperative guidance law with constraints of impact time and impact angle[J]. Journal of Ballistics, 2017, 29(4): 1-8(in Chinese). doi: 10.3969/j.issn.1004-499X.2017.04.001
|
[8] |
YU J L, DONG X W, LI Q D, et al. Cooperative guidance strategy for multiple hypersonic gliding vehicles system[J]. Chinese Journal of Aeronautics, 2020, 33(3): 990-1005. doi: 10.1016/j.cja.2019.12.003
|
[9] |
赵建博, 杨树兴. 多导弹协同制导研究综述[J]. 航空学报, 2017, 38(1): 22-34. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201701002.htm
YANG J B, YANG S X. Review of multi-missile cooperative guidance[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(1): 22-34(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201701002.htm
|
[10] |
王建青, 李帆, 赵建辉, 等. 多导弹协同制导律综述[J]. 飞行力学, 2011, 29(4): 6-10. doi: 10.13645/j.cnki.f.d.2011.04.004
WANG J Q, LI F, ZHAO J H, et al. Summary of guidance law based on cooperative attack of multi-missile method[J]. Flight Dynamics, 2011, 29(4): 6-10(in Chinese). doi: 10.13645/j.cnki.f.d.2011.04.004
|
[11] |
姚禹正, 余文斌, 杨立军, 等. 多导弹协同制导技术综述[J]. 飞航导弹, 2021(6): 112-121. doi: 10.16338/j.issn.1009-1319.20210839
YAO Y Z, YU W B, YANG L J, et al. Overview of multi missile cooperative guidance technology[J]. Aerodynamic Missile Journal, 2021(6): 112-121(in Chinese). doi: 10.16338/j.issn.1009-1319.20210839
|
[12] |
张友安, 王星亮, 吴华丽, 等. 带攻击时间约束的导引律综述[J]. 海军航空工程学院学报, 2015, 30(4): 301-309. https://www.cnki.com.cn/Article/CJFDTOTAL-HJHK201504001.htm
ZHANG Y A, WANG X L, WU H L, et al. Survey of guidance law with attack time constraint[J]. Journal of Naval Aeronautical and Astronautical University, 2015, 30(4): 301-309(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HJHK201504001.htm
|
[13] |
JEON I S, LEE J I, TAHK M J. Impact-time-control guidance law for anti-ship missiles[J]. IEEE Transactions on Control Systems Technology, 2006, 14(2): 260-266. doi: 10.1109/TCST.2005.863655
|
[14] |
赵世钰, 周锐. 基于协调变量的多导弹协同制导[J]. 航空学报, 2008, 29(6): 1605-1611. doi: 10.3321/j.issn:1000-6893.2008.06.031
ZHAO S Y, ZHOU R. Multi-missile cooperative guidance using coordination variables[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(6): 1605-1611(in Chinese). doi: 10.3321/j.issn:1000-6893.2008.06.031
|
[15] |
张春妍, 宋建梅, 侯博, 等. 带落角和时间约束的网络化导弹协同制导律[J]. 兵工学报, 2016, 37(3): 431-438. doi: 10.3969/j.issn.1000-1093.2016.03.007
ZHANG C Y, SONG J M, HOU B, et al. Cooperative guidance law with impact angle and impact time constraints for networked missiles[J]. Acta Armamentarii, 2016, 37(3): 431-438(in Chinese). doi: 10.3969/j.issn.1000-1093.2016.03.007
|
[16] |
JEON I S, LEE J I, TAHK M J. Homing guidance law for cooperative attack of multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(1): 275-280. doi: 10.2514/1.40136
|
[17] |
SINHA A, KUMAR S R, MUKHERJEE D. Cooperative integrated guidance and control design for simultaneous interception[J]. Aerospace Science and Technology, 2022, 120: 107262. doi: 10.1016/j.ast.2021.107262
|
[18] |
LI Z H, DING Z T. Robust cooperative guidance law for simultaneous arrival[J]. IEEE Transactions on Control Systems Technology, 2019, 27(3): 1360-1367. doi: 10.1109/TCST.2018.2804348
|
[19] |
LI K, WANG J N, LEE C H, et al. Distributed cooperative guidance for multivehicle simultaneous arrival without numerical singularities[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(7): 1365-1373. doi: 10.2514/1.G005010
|
[20] |
张友安, 马国欣, 王兴平. 多导弹时间协同制导: 一种领弹-被领弹策略[J]. 航空学报, 2009, 30(6): 1109-1118. doi: 10.3321/j.issn:1000-6893.2009.06.023
ZHANG Y A, MA G X, WANG X P. Time-cooperative guidance for multi-missiles: A leader-follower strategy[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(6): 1109-1118(in Chinese). doi: 10.3321/j.issn:1000-6893.2009.06.023
|
[21] |
林德福, 何绍溟, 王江, 等. 基于虚拟领弹-从弹的集群分布式协同制导技术研究[J]. 中国科学: 技术科学, 2020, 50(5): 506-515. https://www.cnki.com.cn/Article/CJFDTOTAL-JEXK202005003.htm
LIN D F, HE S M, WANG J, et al. Research on cluster distributed collaborative guidance technology based on virtual leader-follower[J]. Scientia Sinica: Technologica, 2020, 50(5): 506-515(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-JEXK202005003.htm
|
[22] |
KORAY S E, RAZIYE T. Impact time and angle control based on constrained optimal solutions[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(10): 2445-2451.
|
[23] |
KANG S, WANG J N, LI G, et al. Optimal cooperative guidance law for salvo attack: An MPC-based consensus perspective[J]. IEEE Transactions on Aerospace and Electronic Systems, 2018, 54(5): 2397-2410. doi: 10.1109/TAES.2018.2816880
|
[24] |
张友根, 张友安, 施建洪, 等. 基于双圆弧原理的协同制导律研究[J]. 海军航空工程学院学报, 2009, 24(5): 537-542. doi: 10.3969/j.issn.1673-1522.2009.05.014
ZHANG Y G, ZHANG Y A, SHI J H, et al. Research on cooperative guidance law based on double arc principle[J]. Journal of Naval Aeronautical and Astronautical University, 2009, 24(5): 537-542(in Chinese). doi: 10.3969/j.issn.1673-1522.2009.05.014
|
[25] |
姜欢, 赵建博, 熊芬芬, 等. 多约束下基于凸优化的协同制导研究[C]//第36届中国控制会议, 2017: 1302-1307.
JIANG H, ZHAO J B, XIONG F F, et al. Cooperative guidance with constrained impact using convex optimization[C]//Proceedings of the 36th Chinese Control Conference, 2017: 1302-1307(in Chinese).
|
[26] |
JIANG H, AN Z, YU Y N, et al. Cooperative guidance with multiple constraints using convex optimization[J]. Aerospace Science and Technology, 2018, 79: 426-440. doi: 10.1016/j.ast.2018.06.001
|
[27] |
CHEN X T, WANG J Z. Nonsingular sliding-mode control for field-of-view constrained impact time guidance[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(5): 1214-1222. doi: 10.2514/1.G003146
|
[28] |
TEKIN R, ERER K S, HOLZAPFEL F. Adaptive impact time control via look-angle shaping under varying velocity[J]. Journal of Guidance, Control, and Dynamics, 2017, 40(12): 3247-3255. doi: 10.2514/1.G002981
|
[29] |
HOU Z W, YANG Y, LIU L, et al. Terminal sliding mode control based impact time and angle constrained guidance[J]. Aerospace Science and Technology, 2019, 93: 105142. doi: 10.1016/j.ast.2019.04.050
|
[30] |
WANG P Y, GUO Y N, MA G F, et al. New look-angle tracking guidance strategy for impact time and angle control[J]. Journal of Guidance, Control, and Dynamics, 2022, 45(3): 545-557. doi: 10.2514/1.G006229
|
[31] |
李浩, 毛昱天, 吴丹, 等. 基于理想视线制导的多导弹协同攻击策略[J]. 导航定位与授时, 2015, 2(4): 1-6. doi: 10.3969/j.issn.2095-8110.2015.04.001
LI H, MAO Y T, WU D, et al. Cooperative attack of multiple missiles with ideal-line-of-sight-guidance[J]. Navigation Positioning and Timing, 2015, 2(4): 1-6(in Chinese). doi: 10.3969/j.issn.2095-8110.2015.04.001
|
[32] |
李斌, 林德福, 何绍溟, 等. 基于最优误差动力学的时间角度控制制导律[J]. 航空学报, 2018, 39(11): 157-167. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201811014.htm
LI B, LIN D F, HE S M, et al. Time and angle control guidance law based on optimal error dynamics[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(11): 157-167(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201811014.htm
|
[33] |
WANG C, DONG W, WANG J, et al. Guidance law design with fixed-time convergent error dynamics[J]. Journal of Guidance, Control, and Dynamics, 2021, 44(7): 1389-1398. doi: 10.2514/1.G005833
|
[34] |
ZHOU J L, YANG J Y. Distributed guidance law design for cooperative simultaneous attacks with multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(10): 2439-2447. doi: 10.2514/1.G001609
|
[35] |
李国飞, 朱国梁, 吕金虎, 等. 主-从多飞行器三维分布式协同制导方法[J]. 航空学报, 2021, 42(11): 236-245. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB202111016.htm
LI G F, ZHU G L, LU J H, et al. Three-dimensional distributive cooperative guidance law for multiple leader-follower flight vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(11): 236-245(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB202111016.htm
|
[36] |
CHEN Y D, WANG J N, SHAN J Y, et al. Cooperative guidance for multiple powered missiles with constrained impact and bounded speed[J]. Journal of Guidance, Control, and Dynamics, 2021, 44(4): 825-841. doi: 10.2514/1.G005578
|
[37] |
WANG X H, TAN C P. 3-D impact angle constrained distributed cooperative guidance for maneuvering targets without angular-rate measurements[J]. Control Engineering Practice, 2018, 78: 142-159. doi: 10.1016/j.conengprac.2018.06.014
|
[38] |
LYU T, LI C J, GUO Y N, et al. Three-dimensional finite-time cooperative guidance for multiple missiles without radial velocity measurements[J]. Chinese Journal of Aeronautics, 2019, 32(5): 1294-1304. doi: 10.1016/j.cja.2018.12.005
|
[39] |
方洋旺, 邓天博, 符文星. 智能制导律研究综述[J]. 无人系统技术, 2020, 3(6): 36-42. https://www.cnki.com.cn/Article/CJFDTOTAL-UMST202006004.htm
FANG Y W, DENG T B, FU W X. An overview on the intelligent guidance law[J]. Unmanned Systems Technology, 2020, 3(6): 36-42(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-UMST202006004.htm
|
[40] |
金泽宇, 刘凯, 尹中杰, 等. 基于神经网络剩余时间模型的协同制导律设计[J]. 战术导弹技术, 2021(4): 103-109. https://www.cnki.com.cn/Article/CJFDTOTAL-ZSDD202104011.htm
JIN Z Y, LIU K, YIN Z J, et al. Impact time cooperation guidance law design based on time-to-go estimating model using neural network[J]. Tactical Missile Technology, 2021(4): 103-109(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-ZSDD202104011.htm
|
[41] |
陈中原, 韦文书, 陈万春. 基于强化学习的多发导弹协同攻击智能制导律[J]. 兵工学报, 2021, 42(8): 1638-1647. doi: 10.3969/j.issn.1000-1093.2021.08.008
CHEN Z Y, WEI W S, CHEN W C. Reinforcement learning-based intelligent guidance law for cooperative attack of multiple missiles[J]. Acta Armamentarii, 2021, 42(8): 1638-1647(in Chinese). doi: 10.3969/j.issn.1000-1093.2021.08.008
|
[42] |
蔡远利, 闫明明, 刘佳琪. 基于深度强化学习的时间协同制导方法及仿真[C]//第22届中国系统仿真技术及其应用学术年会, 2021: 371-375.
CAI Y L, YAN M M, LIU J Q. Research on deep reinforcement learning based temporal cooperative guidance method and simulation[C]//22nd CCSSTA, 2021: 371-375(in Chinese).
|
[43] |
周华, 刘红军, 王泽, 等. 一种基于目标机动补偿的协同制导律[J]. 导弹与航天运载技术, 2015(1): 92-95. https://www.cnki.com.cn/Article/CJFDTOTAL-DDYH201501027.htm
ZHOU H, LIU H J, WANG Z, et al. Synergistic guidance law based on target maneuvering compensation[J]. Missiles And Space Vehicles, 2015(1): 92-95(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-DDYH201501027.htm
|
[44] |
马萌晨, 宋申民. 拦截机动目标的多导弹协同制导律[J]. 航空兵器, 2021, 28(6): 19-27. https://www.cnki.com.cn/Article/CJFDTOTAL-HKBQ202106004.htm
MA M C, SONG S M. Multi-missile cooperative guidance law for intercepting maneuvering target[J]. Aero Weaponry, 2021, 28(6): 19-27(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKBQ202106004.htm
|
[45] |
KUMAR S R, MUKHERJEE D. Terminal time constrained nonlinear interception strategies against maneuvering targets[J]. Journal Guidance, Control, and Dynamics, 2021, 44(1): 200-209.
|
[46] |
BISHWASH H U S, SINHA A, KUMAR S R. Deviated pursuit based nonlinear impact-time guidance with finite-time convergence[J]. International Federation of Automatic Control, 2020, 53(1): 93-98.
|
[47] |
张保峰. 带攻击角度约束的多导弹协同导引律设计[D]. 哈尔滨: 哈尔滨工业大学, 2013: 35-47.
ZHANG B F. Design of multi-missile cooperative guidance law with attack angle constraint[D]. Harbin: Harbin Institute of Technology, 2013: 35-47(in Chinese).
|
[48] |
FONOD R, SHIMA T. Blinding guidance against missiles sharing bearings-only measurements[J]. IEEE Transactions on Aerospace and Electronic Systems, 2018, 54(1): 205-216.
|
[49] |
杨雪冬, 朱蕊蘋, 李君龙. 交会时间可控的多子弹协同制导方法[J]. 现代防御技术, 2013, 41(1): 59-63. https://www.cnki.com.cn/Article/CJFDTOTAL-XDFJ201301011.htm
YNAG X D, ZHU R P, LI Y L. Submunitions cooperative guidance method of controllable rendezvous time[J]. Modern Defence Technology, 2013, 41(1): 59-63(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-XDFJ201301011.htm
|
[50] |
TSALIK R, SHIMA T. Circular impact-time guidance[J]. Journal of Guidance, Control, and Dymaics, 2019, 42(8): 1836-1847.
|
[51] |
CHO D, KIM H J. Nonsingular sliding mode guidance for impact time control[J]. Journal of Guidance, Control, and Dymaics, 2016, 39(1): 61-68.
|
[52] |
CHO N, LEE Y I. Guidance synthesis with separate impact point prediction considering speed variations[J]. Journal of Guidance, Control, and Dymaics, 2021, 44(2): 428-440.
|
[53] |
HU Q L, HAN T. New impact time and angle guidance strategy via virtual target approach[J]. Journal of Guidance, Control, and Dymaics, 2018, 41(8): 1755-1765.
|
[54] |
TEKIN R, ERER K S. Impact time and angle control against moving targets with look angle shaping[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(5): 1020-1025.
|
[55] |
SINHA A, KUMAR S R, MUKHERJEE D. Nonsingular impact time guidance and control using deviated pursuit[J]. Aerospace Science and Technology, 2021, 115: 106776. doi: 10.1016/j.ast.2021.106776
|
[56] |
张友安, 梁勇, 刘京茂, 等. 基于轨迹成型的攻击角度与时间控制[J]. 航空学报, 2018, 39(9): 138-146. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201809013.htm
ZHANG Y A, LIANG Y, LIU J M, et al. Trajectory reshaping based impact angle and time control[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(9): 138-146(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201809013.htm
|
[57] |
HU Q L, HAN T, XIN M. Sliding-mode impact time guidance law design for various target motions[J]. Journal of Guidance, Control, and Dynamics, 2019, 42(1): 136-148.
|
[58] |
吕腾, 吕跃勇, 李传江, 等. 带空间协同的多导弹时间协同制导律[J]. 航空学报, 2018, 39(10): 185-196. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201810015.htm
LYU T, LYU Y Y, LI C J, et al. Time cooperative guidance law for multiple missiles with spatial cooperation[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(10): 185-196(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201810015.htm
|
[59] |
DONG W, WANG C, WANG J, et al. Fixed-time terminal angle constrained cooperative guidance law against maneuvering target[J]. IEEE Transactions on Aerospace and Electronic Systems, 2022, 58(2): 1352-1366.
|
[60] |
赵恩娇. 多飞行器编队控制及协同制导方法[D]. 哈尔滨: 哈尔滨工业大学, 2018: 70-95.
ZHAO E J. Formation control and cooperative guidance methods for multiple flight vehicles[D]. Harbin: Harbin Institute of Technology, 2018: 70-95(in Chinese).
|
[61] |
宋俊红. 拦截机动目标的有限时间制导律及多弹协同制导律研究[D]. 哈尔滨: 哈尔滨工业大学, 2018: 124-146.
SONG J H. Research on finite-time guidance law and cooperative guidance law of multi-missiles for intercepting maneuvering target[D]. Harbin: Harbin Institute of Technology, 2018: 124-146(in Chinese).
|
[62] |
ZHANG S, GUO Y, LIU Z, et al. Finite-time cooperative guidance strategy for impact angle and time control[J]. IEEE Transactions on Aerospace and Electronic Systems, 2021, 57(2): 806-819. doi: 10.1109/TAES.2020.3037958
|
[63] |
ZHANG P, ZHANG X. Multiple missiles fixed-time cooperative guidance without measuring radial velocity for maneuvering targets interception[J]. ISA Transactions, 2022, 126: 388-397. doi: 10.1016/j.isatra.2021.07.023
|
[64] |
TAN Z W, FONOD R, SHIMA T. Cooperative guidance law for target pair to lure two pursuers into collision[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(8): 1687-1699.
|
[65] |
袁斐然, 刘春生, 陈必露. 基于自适应动态规划的多对一追逃博弈策略[J]. 电光与控制, 2022, 29(1): 1-6. https://www.cnki.com.cn/Article/CJFDTOTAL-DGKQ202201001.htm
YUAN F R, LIU C S, CHEN B L. Many-to-one pursuit-evasion game strategy based on adaptive dynamic programming[J]. Electronics Optics & Control, 2022, 29(1): 1-6(in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-DGKQ202201001.htm
|
[66] |
孙景亮. 自适应动态规划研究及其在导弹拦截制导中的应用[D]. 南京: 南京航空航天大学, 2019: 77-89.
SUN J L. Research on adaptive dynamic programming and its applications to the missile interception guidance[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019: 77-89(in Chinese).
|
[67] |
LONG T, CAO Y, SUN J L, et al. Adaptive event-triggered distributed optimal guidance design via adaptive dynamic programming[J]. Chinese Journal of Aeronautics, 2022, 35(7): 113-127.
|